The best brief description of the Langley aerodrome in its final form,

and of the two attempted trials, is contained in the official report of

Major M. M. Macomb of the United States Artillery Corps, which report is

here given in full:--

REPORT

Experiments with working models which were concluded August 8 last

having proved the principles and calculations on which the design of the

Langley aerodrome was based to be correct, the next step was to apply

these principles to the construction of a machine of sufficient size

and power to permit the carrying of a man, who could control the motive

power and guide its flight, thus pointing the way to attaining the final

goal of producing a machine capable of such extensive and precise aerial

flight, under normal atmospheric conditions, as to prove of military or

commercial utility.

Mr C. M. Manly, working under Professor Langley, had, by the summer

of 1903, succeeded in completing an engine-driven machine which under

favourable atmospheric conditions was expected to carry a man for any

time up to half an hour, and to be capable of having its flight directed

and controlled by him.

The supporting surface of the wings was ample, and experiment showed the

engine capable of supplying more than the necessary motive power.

Owing to the necessity of lightness, the weight of the various elements

had to be kept at a minimum, and the factor of safety in construction

was therefore exceedingly small, so that the machine as a whole was

delicate and frail and incapable of sustaining any unusual strain. This

defect was to be corrected in later models by utilising data gathered in

future experiments under varied conditions.

One of the most remarkable results attained was the production of a

gasoline engine furnishing over fifty continuous horse-power for a

weight of 120 lbs.

The aerodrome, as completed and prepared for test, is briefly described

by Professor Langley as 'built of steel, weighing complete about

730 lbs., supported by 1,040 feet of sustaining surface, having two

propellers driven by a gas engine developing continuously over fifty

brake horse-power.'

The appearance of the machine prepared for flight was exceedingly light

and graceful, giving an impression to all observers of being capable of

successful flight.

On October 7 last everything was in readiness, and I witnessed the

attempted trial on that day at Widewater, Va. On the Potomac. The engine

worked well and the machine was launched at about 12.15 p.m. The trial

was unsuccessful because the front guy-post caught in its support on the

launching car and was not released in time to give free flight, as was

intended, but, on the contrary, caused the front of the machine to be

dragged downward, bending the guy-post and making the machine plunge

into the water about fifty yards in front of the house-boat. The machine

was subsequently recovered and brought back to the house-boat. The

engine was uninjured and the frame only slightly damaged, but the four

wings and rudder were practically destroyed by the first plunge and

subsequent towing back to the house-boat.

This accident necessitated the removal of the house-boat to Washington

for the more convenient repair of damages.

On December 8 last, between 4 and 5 p.m., another attempt at a trial was

made, this time at the junction of the Anacostia with the Potomac, just

below Washington Barracks.

On this occasion General Randolph and myself represented the Board of

Ordnance and Fortification. The launching car was released at 4.45 p.m.

being pointed up the Anacostia towards the Navy Yard. My position was

on the tug Bartholdi, about 150 feet from and at right angles to

the direction of proposed flight. The car was set in motion and the

propellers revolved rapidly, the engine working perfectly, but there was

something wrong with the launching. The rear guy-post seemed to drag,

bringing the rudder down on the launching ways, and a crashing, rending

sound, followed by the collapse of the rear wings, showed that the

machine had been wrecked in the launching, just how, it was impossible

for me to see. The fact remains that the rear wings and rudder were

wrecked before the machine was free of the ways. Their collapse deprived

the machine of its support in the rear, and it consequently reared up

in front under the action of the motor, assumed a vertical position,

and then toppled over to the rear, falling into the water a few feet in

front of the boat.

Mr Manly was pulled out of the wreck uninjured and the wrecked

machine--was subsequently placed upon the house-boat, and the whole

brought back to Washington.

From what has been said it will be seen that these unfortunate accidents

have prevented any test of the apparatus in free flight, and the claim

that an engine-driven, man-carrying aerodrome has been constructed lacks

the proof which actual flight alone can give.

Having reached the present stage of advancement in its development, it

would seem highly desirable, before laying down the investigation, to

obtain conclusive proof of the possibility of free flight, not only

because there are excellent reasons to hope for success, but because

it marks the end of a definite step toward the attainment of the final

goal.

Just what further procedure is necessary to secure successful flight

with the large aerodrome has not yet been decided upon. Professor

Langley is understood to have this subject under advisement, and

will doubtless inform the Board of his final conclusions as soon as

practicable.

In the meantime, to avoid any possible misunderstanding, it should be

stated that even after a successful test of the present great aerodrome,

designed to carry a man, we are still far from the ultimate goal, and it

would seem as if years of constant work and study by experts, together

with the expenditure of thousands of dollars, would still be necessary

before we can hope to produce an apparatus of practical utility on these

lines.--Washington, January 6, 1904.

A subsequent report of the Board of ordnance and Fortification to the

Secretary of War embodied the principal points in Major Macomb's report,

but as early as March 3rd, 1904, the Board came to a similar conclusion

to that of the French Ministry of War in respect of Clement Ader's work,

stating that it was not 'prepared to make an additional allotment

at this time for continuing the work.' This decision was in no small

measure due to hostile newspaper criticisms. Langley, in a letter to

the press explaining his attitude, stated that he did not wish to make

public the results of his work till these were certain, in consequence

of which he refused admittance to newspaper representatives, and this

attitude produced a hostility which had effect on the United States

Congress. An offer was made to commercialise the invention, but Langley

steadfastly refused it. Concerning this, Manly remarks that Langley

had 'given his time and his best labours to the world without hope of

remuneration, and he could not bring himself, at his stage of life, to

consent to capitalise his scientific work.'

The final trial of the Langley aerodrome was made on December 8th, 1903;

nine days later, on December 17th, the Wright Brothers made their first

flight in a power-propelled machine, and the conquest of the air was

thus achieved. But for the two accidents that spoilt his trials, the

honour which fell to the Wright Brothers would, beyond doubt, have been

secured by Samuel Pierpoint Langley.

XI. THE WRIGHT BROTHERS

Such information as is given here concerning the Wright Brothers is

derived from the two best sources available, namely, the writings of

Wilbur Wright himself, and a lecture given by Dr Griffith Brewer to

members of the Royal Aeronautical Society. There is no doubt that so

far as actual work in connection with aviation accomplished by the two

brothers is concerned, Wilbur Wright's own statements are the clearest

and best available. Apparently Wilbur was, from the beginning, the

historian of the pair, though he himself would have been the last to

attempt to detract in any way from the fame that his brother's work also

deserves. Throughout all their experiments the two were inseparable,

and their work is one indivisible whole; in fact, in every department

of that work, it is impossible to say where Orville leaves off and where

Wilbur begins.

It is a great story, this of the Wright Brothers, and one worth all the

detail that can be spared it. It begins on the 16th April, 1867, when

Wilbur Wright was born within eight miles of Newcastle, Indiana. Before

Orville's birth on the 19th August, 1871, the Wright family had moved

to Dayton, Ohio, and settled on what is known as the 'West Side' of the

town. Here the brothers grew up, and, when Orville was still a boy in

his teens, he started a printing business, which, as Griffith Brewer

remarks, was only limited by the smallness of his machine and small

quantity of type at his disposal. This machine was in such a state that

pieces of string and wood were incorporated in it by way of repair, but

on it Orville managed to print a boys' paper which gained considerable

popularity in Dayton 'West Side.' Later, at the age of seventeen,

he obtained a more efficient outfit, with which he launched a weekly

newspaper, four pages in size, entitled The West Side News. After three

months' running the paper was increased in size and Wilbur came into

the enterprise as editor, Orville remaining publisher. In 1894 the two

brothers began the publication of a weekly magazine, Snap-Shots, to

which Wilbur contributed a series of articles on local affairs that gave

evidence of the incisive and often sarcastic manner in which he was able

to express himself throughout his life. Dr Griffith Brewer describes him

as a fearless critic, who wrote on matters of local interest in a kindly

but vigorous manner, which did much to maintain the healthy public

municipal life of Dayton.

Editorial and publishing enterprise was succeeded by the formation, just

across the road from the printing works, of the Wright Cycle Company,

where the two brothers launched out as cycle manufacturers with the

'Van Cleve' bicycle, a machine of great local repute for excellence of

construction, and one which won for itself a reputation that lasted long

after it had ceased to be manufactured. The name of the machine was that

of an ancestor of the brothers, Catherine Van Cleve, who was one of the

first settlers at Dayton, landing there from the River Miami on April

1st, 1796, when the country was virgin forest.

It was not until 1896 that the mechanical genius which characterised

the two brothers was turned to the consideration of aeronautics. In that

year they took up the problem thoroughly, studying all the aeronautical

information then in print. Lilienthal's writings formed one basis for

their studies, and the work of Langley assisted in establishing in

them a confidence in the possibility of a solution to the problems of

mechanical flight. In 1909, at the banquet given by the Royal Aero Club

to the Wright Brothers on their return to America, after the series of

demonstration flights carried out by Wilbur Wright on the Continent,

Wilbur paid tribute to the great pioneer work of Stringfellow, whose

studies and achievements influenced his own and Orville's early work. He

pointed out how Stringfellow devised an aeroplane having two propellers

and vertical and horizontal steering, and gave due place to this early

pioneer of mechanical flight.

Neither of the brothers was content with mere study of the work of

others. They collected all the theory available in the books published

up to that time, and then built man-carrying gliders with which to test

the data of Lilienthal and such other authorities as they had consulted.

For two years they conducted outdoor experiments in order to test the

truth or otherwise of what were enunciated as the principles of flight;

after this they turned to laboratory experiments, constructing a wind

tunnel in which they made thousands of tests with models of various

forms of curved planes. From their experiments they tabulated thousands

of readings, which Griffith Brewer remarks as giving results equally

efficient with those of the elaborate tables prepared by learned

institutions.

Wilbur Wright has set down the beginnings of the practical experiments

made by the two brothers very clearly. 'The difficulties,' he says,

'which obstruct the pathway to success in flying machine construction

are of three general classes: (1) Those which relate to the construction

of the sustaining wings; (2) those which relate to the generation and

application of the power required to drive the machine through the air;

(3) those relating to the balancing and steering of the machine after

it is actually in flight. Of these difficulties two are already to

a certain extent solved. Men already know how to construct wings, or

aeroplanes, which, when driven through the air at sufficient speed, will

not only sustain the weight of the wings themselves, but also that of

the engine and the engineer as well. Men also know how to build engines

and' screws of sufficient lightness and power to drive these planes

at sustaining speed. Inability to balance and steer still confronts

students of the flying problem, although nearly ten years have passed

(since Lilienthal's success). When this one feature has been worked out,

the age of flying machines will have arrived, for all other difficulties

are of minor importance.

'The person who merely watches the flight of a bird gathers the

impression that the bird has nothing to think of but the flapping of

its wings. As a matter of fact, this is a very small part of its mental

labour. Even to mention all the things the bird must constantly keep in

mind in order to fly securely through the air would take a considerable

time. If I take a piece of paper and, after placing it parallel with

the ground, quickly let it fall, it will not settle steadily down as

a staid, sensible piece of paper ought to do, but it insists on

contravening every recognised rule of decorum, turning over and darting

hither and thither in the most erratic manner, much after the style of

an untrained horse. Yet this is the style of steed that men must learn

to manage before flying can become an everyday sport. The bird has

learned this art of equilibrium, and learned it so thoroughly that its

skill is not apparent to our sight. We only learn to appreciate it when

we can imitate it.

'Now, there are only two ways of learning to ride a fractious horse: one

is to get on him and learn by actual practice how each motion and trick

may be best met; the other is to sit on a fence and watch the beast

awhile, and then retire to the house and at leisure figure out the best

way of overcoming his jumps and kicks. The latter system is the safer,

but the former, on the whole, turns out the larger proportion of good

riders. It is very much the same in learning to ride a flying machine;

if you are looking for perfect safety you will do well to sit on a fence

and watch the birds, but if you really wish to learn you must mount

a machine and become acquainted with its tricks by actual trial. The

balancing of a gliding or flying machine is very simple in theory. It

merely consists in causing the centre of pressure to coincide with the

centre of gravity.'

These comments are taken from a lecture delivered by Wilbur Wright

before the Western Society of Engineers in September of 1901, under the

presidency of Octave Chanute. In that lecture Wilbur detailed the way

in which he and his brother came to interest themselves in aeronautical

problems and constructed their first glider. He speaks of his own

notice of the death of Lilienthal in 1896, and of the way in which this

fatality roused him to an active interest in aeronautical problems,

which was stimulated by reading Professor Marey's Animal Mechanism, not

for the first time. 'From this I was led to read more modern works, and

as my brother soon became equally interested with myself, we soon passed

from the reading to the thinking, and finally to the working stage. It

seemed to us that the main reason why the problem had remained so long

unsolved was that no one had been able to obtain any adequate practice.

We figured that Lilienthal in five years of time had spent only about

five hours in actual gliding through the air. The wonder was not that he

had done so little, but that he had accomplished so much. It would not

be considered at all safe for a bicycle rider to attempt to ride through

a crowded city street after only five hours' practice, spread out in

bits of ten seconds each over a period of five years; yet Lilienthal

with this brief practice was remarkably successful in meeting the

fluctuations and eddies of wind-gusts. We thought that if some method

could be found by which it would be possible to practice by the hour

instead of by the second there would be hope of advancing the solution

of a very difficult problem. It seemed feasible to do this by building a

machine which would be sustained at a speed of eighteen miles per hour,

and then finding a locality where winds of this velocity were common.

With these conditions a rope attached to the machine to keep it from

floating backward would answer very nearly the same purpose as a

propeller driven by a motor, and it would be possible to practice by the

hour, and without any serious danger, as it would not be necessary to

rise far from the ground, and the machine would not have any forward

motion at all. We found, according to the accepted tables of air

pressure on curved surfaces, that a machine spreading 200 square feet of

wing surface would be sufficient for our purpose, and that places would

easily be found along the Atlantic coast where winds of sixteen to

twenty-five miles were not at all uncommon. When the winds were low it

was our plan to glide from the tops of sandhills, and when they were

sufficiently strong to use a rope for our motor and fly over one spot.

Our next work was to draw up the plans for a suitable machine. After

much study we finally concluded that tails were a source of trouble

rather than of assistance, and therefore we decided to dispense with

them altogether. It seemed reasonable that if the body of the operator

could be placed in a horizontal position instead of the upright, as in

the machines of Lilienthal, Pilcher, and Chanute, the wind resistance

could be very materially reduced, since only one square foot instead of

five would be exposed. As a full half horse-power would be saved by this

change, we arranged to try at least the horizontal position. Then the

method of control used by Lilienthal, which consisted in shifting the

body, did not seem quite as quick or effective as the case required; so,

after long study, we contrived a system consisting of two large surfaces

on the Chanute double-deck plan, and a smaller surface placed a short

distance in front of the main surfaces in such a position that the

action of the wind upon it would counterbalance the effect of the travel

of the centre of pressure on the main surfaces. Thus changes in the

direction and velocity of the wind would have little disturbing effect,

and the operator would be required to attend only to the steering of the

machine, which was to be effected by curving the forward surface up or

down. The lateral equilibrium and the steering to right or left was

to be attained by a peculiar torsion of the main surfaces which was

equivalent to presenting one end of the wings at a greater angle than

the other. In the main frame a few changes were also made in the details

of construction and trussing employed by Mr Chanute. The most important

of these were: (1) The moving of the forward main crosspiece of the

frame to the extreme front edge; (2) the encasing in the cloth of all

crosspieces and ribs of the surfaces; (3) a rearrangement of the wires

used in trussing the two surfaces together, which rendered it possible

to tighten all the wires by simply shortening two of them.'

The brothers intended originally to get 200 square feet of supporting

surface for their glider, but the impossibility of obtaining suitable

material compelled them to reduce the area to 165 square feet, which, by

the Lilienthal tables, admitted of support in a wind of about twenty-one

miles an hour at an angle of three degrees. With this glider they went

in the summer of I 1900 to the little settlement of Kitty Hawk, North

Carolina, situated on the strip of land dividing Albemarle Sound from

the Atlantic. Here they reckoned on obtaining steady wind, and here, on

the day that they completed the machine, they took it out for trial as

a kite with the wind blowing at between twenty-five and thirty miles

an hour. They found that in order to support a man on it the glider

required an angle nearer twenty degrees than three, and even with the

wind at thirty miles an hour they could not get down to the planned

angle of three degrees. 'Later, when the wind was too light to support

the machine with a man on it, they tested it as a kite, working the

rudders by cords. Although they obtained satisfactory results in this

way they realised fully that actual gliding experience was necessary

before the tests could be considered practical.

A series of actual measurements of lift and drift of the machine gave

astonishing results. 'It appeared that the total horizontal pull of the

machine, while sustaining a weight of 52 lbs., was only 8.5 lbs., which

was less than had been previously estimated for head resistance of the

framing alone. Making allowance for the weight carried, it appeared that

the head resistance of the framing was but little more than fifty per

cent of the amount which Mr Chanute had estimated as the head resistance

of the framing of his machine. On the other hand, it appeared sadly

deficient in lifting power as compared with the calculated lift of

curved surfaces of its size... we decided to arrange our machine for the

following year so that the depth of curvature of its surfaces could be

varied at will, and its covering air-proofed.'

After these experiments the brothers decided to turn to practical

gliding, for which they moved four miles to the south, to the Kill Devil

sandhills, the principal of which is slightly over a hundred feet

in height, with an inclination of nearly ten degrees on its main

north-western slope. On the day after their arrival they made about a

dozen glides, in which, although the landings were made at a speed of

more than twenty miles an hour, no injury was sustained either by the

machine or by the operator.

'The slope of the hill was 9.5 degrees, or a drop of one foot in six. We

found that after attaining a speed of about twenty-five to thirty miles

with reference to the wind, or ten to fifteen miles over the ground, the

machine not only glided parallel to the slope of the hill, but greatly

increased its speed, thus indicating its ability to glide on a somewhat

less angle than 9.5 degrees, when we should feel it safe to rise higher

from the surface. The control of the machine proved even better than we

had dared to expect, responding quickly to the slightest motion of the

rudder. With these glides our experiments for the year 1900 closed.

Although the hours and hours of practice we had hoped to obtain finally

dwindled down to about two minutes, we were very much pleased with the

general results of the trip, for, setting out as we did with almost

revolutionary theories on many points and an entirely untried form of

machine, we considered it quite a point to be able to return without

having our pet theories completely knocked on the head by the hard logic

of experience, and our own brains dashed out in the bargain. Everything

seemed to us to confirm the correctness of our original opinions:

(1) That practice is the key to the secret of flying; (2) that it

is practicable to assume the horizontal position; (3) that a smaller

surface set at a negative angle in front of the main bearing surfaces,

or wings, will largely counteract the effect of the fore and aft travel

of the centre of pressure; (4) that steering up and down can be attained

with a rudder without moving the position of the operator's body; (5)

that twisting the wings so as to present their ends to the wind at

different angles is a more prompt and efficient way of maintaining

lateral equilibrium than shifting the body of the operator.'

For the gliding experiments of 1901 it was decided to retain the form of

the 1900 glider, but to increase the area to 308 square feet, which, the

brothers calculated, would support itself and its operator in a wind

of seventeen miles an hour with an angle of incidence of three degrees.

Camp was formed at Kitty Hawk in the middle of July, and on July 27th

the machine was completed and tried for the first time in a wind of

about fourteen miles an hour. The first attempt resulted in landing

after a glide of only a few yards, indicating that the centre of gravity

was too far in front of the centre of pressure. By shifting his position

farther and farther back the operator finally achieved an undulating

flight of a little over 300 feet, but to obtain this success he had to

use full power of the rudder to prevent both stalling and nose-diving.

With the 1900 machine one-fourth of the rudder action had been necessary

for far better control.

Practically all glides gave the same result, and in one the machine rose

higher and higher until it lost all headway. 'This was the position from

which Lilienthal had always found difficulty in extricating himself,

as his machine then, in spite of his greatest exertions, manifested a

tendency to dive downward almost vertically and strike the ground head

on with frightful velocity. In this case a warning cry from the ground

caused the operator to turn the rudder to its full extent and also to

move his body slightly forward. The machine then settled slowly to the

ground, maintaining its horizontal position almost perfectly, and landed

without any injury at all. This was very encouraging, as it showed that

one of the very greatest dangers in machines with horizontal tails had

been overcome by the use of the front rudder. Several glides later the

same experience was repeated with the same result. In the latter case

the machine had even commenced to move backward, but was nevertheless

brought safely to the ground in a horizontal position. On the whole this

day's experiments were encouraging, for while the action of the rudder

did not seem at all like that of our 1900 machine, yet we had escaped

without difficulty from positions which had proved very dangerous

to preceding experimenters, and after less than one minute's actual

practice had made a glide of more than 300 feet, at an angle of

descent of ten degrees, and with a machine nearly twice as large as had

previously been considered safe. The trouble with its control, which

has been mentioned, we believed could be corrected when we should have

located its cause.'

It was finally ascertained that the defect could be remedied by

trussing down the ribs of the whole machine so as to reduce the depth of

curvature. When this had been done gliding was resumed, and after a few

trials glides of 366 and 389 feet were made with prompt response on the

part of the machine, even to small movements of the rudder. The rest of

the story of the gliding experiments of 1901 cannot be better told than

in Wilbur Wright's own words, as uttered by him in the lecture from

which the foregoing excerpts have been made.

'The machine, with its new curvature, never failed to respond promptly

to even small movements of the rudder. The operator could cause it to

almost skim the ground, following the undulations of its surface, or he

could cause it to sail out almost on a level with the starting point,

and, passing high above the foot of the hill, gradually settle down to

the ground. The wind on this day was blowing eleven to fourteen miles

per hour. The next day, the conditions being favourable, the machine

was again taken out for trial. This time the velocity of the wind was

eighteen to twenty-two miles per hour. At first we felt some doubt as to

the safety of attempting free flight in so strong a wind, with a machine

of over 300 square feet and a practice of less than five minutes spent

in actual flight. But after several preliminary experiments we decided

to try a glide. The control of the machine seemed so good that we then

felt no apprehension in sailing boldly forth. And thereafter we made

glide after glide, sometimes following the ground closely and sometimes

sailing high in the air. Mr Chanute had his camera with him and took

pictures of some of these glides, several of which are among those

shown.

'We made glides on subsequent days, whenever the conditions were

favourable. The highest wind thus experimented in was a little over

twelve metres per second--nearly twenty-seven miles per hour.

It had been our intention when building the machine to do the larger

part of the experimenting in the following manner:--When the wind blew

seventeen miles an hour, or more, we would attach a rope to the machine

and let it rise as a kite with the operator upon it. When it should

reach a proper height the operator would cast off the rope and glide

down to the ground just as from the top of a hill. In this way we would

be saved the trouble of carrying the machine uphill after each glide,

and could make at least ten glides in the time required for one in the

other way. But when we came to try it, we found that a wind of seventeen

miles, as measured by Richards' anemometer, instead of sustaining the

machine with its operator, a total weight of 240 lbs., at an angle of

incidence of three degrees, in reality would not sustain the machine

alone--100 lbs.--at this angle. Its lifting capacity seemed scarcely one

third of the calculated amount. In order to make sure that this was not

due to the porosity of the cloth, we constructed two small experimental

surfaces of equal size, one of which was air-proofed and the other left

in its natural state; but we could detect no difference in their lifting

powers. For a time we were led to suspect that the lift of curved

surfaces very little exceeded that of planes of the same size, but

further investigation and experiment led to the opinion that (1) the

anemometer used by us over-recorded the true velocity of the wind by

nearly 15 per cent; (2) that the well-known Smeaton co-efficient of.005

V squared for the wind pressure at 90 degrees is probably too great by

at least 20 per cent; (3) that Lilienthal's estimate that the pressure

on a curved surface having an angle of incidence of 3 degrees equals.545

of the pressure at go degrees is too large, being nearly 50 per

cent greater than very recent experiments of our own with a pressure

testing-machine indicate; (4) that the superposition of the surfaces

somewhat reduced the lift per square foot, as compared with a single

surface of equal area.

'In gliding experiments, however, the amount of lift is of less relative

importance than the ratio of lift to drift, as this alone decides

the angle of gliding descent. In a plane the pressure is always

perpendicular to the surface, and the ratio of lift to drift is

therefore the same as that of the cosine to the sine of the angle of

incidence. But in curved surfaces a very remarkable situation is found.

The pressure, instead of being uniformly normal to the chord of the

arc, is usually inclined considerably in front of the perpendicular.

The result is that the lift is greater and the drift less than if

the pressure were normal. Lilienthal was the first to discover this

exceedingly important fact, which is fully set forth in his book, Bird

Flight the Basis of the Flying Art, but owing to some errors in the

methods he used in making measurements, question was raised by other

investigators not only as to the accuracy of his figures, but even as

to the existence of any tangential force at all. Our experiments confirm

the existence of this force, though our measurements differ considerably

from those of Lilienthal. While at Kitty Hawk we spent much time in

measuring the horizontal pressure on our unloaded machine at various

angles of incidence. We found that at 13 degrees the horizontal pressure

was about 23 lbs. This included not only the drift proper, or horizontal

component of the pressure on the side of the surface, but also the head

resistance of the framing as well. The weight of the machine at the time

of this test was about 108 lbs. Now, if the pressure had been normal to

the chord of the surface, the drift proper would have been to the lift

(108 lbs.) as the sine of 13 degrees is to the cosine of 13 degrees,

or.22 X 108/.97 = 24+ lbs.; but this slightly exceeds the total pull

of 23 pounds on our scales. Therefore it is evident that the average

pressure on the surface, instead of being normal to the chord, was so

far inclined toward the front that all the head resistance of framing

and wires used in the construction was more than overcome. In a wind of

fourteen miles per hour resistance is by no means a negligible factor,

so that tangential is evidently a force of considerable value. In a

higher wind, which sustained the machine at an angle of 10 degrees the

pull on the scales was 18 lbs. With the pressure normal to the chord the

drift proper would have been 17 X 98/.98. The travel of the centre of

pressure made it necessary to put sand on the front rudder to bring

the centres of gravity and pressure into coincidence, consequently the

weight of the machine varied from 98 lbs. to 108 lbs. in the different

tests= 17 lbs., so that, although the higher wind velocity must have

caused an increase in the head resistance, the tangential force still

came within 1 lb. of overcoming it. After our return from Kitty Hawk

we began a series of experiments to accurately determine the amount and

direction of the pressure produced on curved surfaces when acted upon by

winds at the various angles from zero to 90 degrees. These experiments

are not yet concluded, but in general they support Lilienthal in the

claim that the curves give pressures more favourable in amount and

direction than planes; but we find marked differences in the exact

values, especially at angles below 10 degrees. We were unable to obtain

direct measurements of the horizontal pressures of the machine with

the operator on board, but by comparing the distance travelled with the

vertical fall, it was easily calculated that at a speed of 24 miles per

hour the total horizontal resistances of our machine, when bearing

the operator, amounted to 40 lbs., which is equivalent to about 2 1/3

horse-power. It must not be supposed, however, that a motor developing

this power would be sufficient to drive a man-bearing machine. The extra

weight of the motor would require either a larger machine, higher speed,

or a greater angle of incidence in order to support it, and therefore

more power. It is probable, however, that an engine of 6 horse-power,

weighing 100 lbs. would answer the purpose. Such an engine is entirely

practicable. Indeed, working motors of one-half this weight per

horse-power (9 lbs. per horse-power) have been constructed by several

different builders. Increasing the speed of our machine from 24 to 33

miles per hour reduced the total horizontal pressure from 40 to about 35

lbs. This was quite an advantage in gliding, as it made it possible to

sail about 15 per cent farther with a given drop. However, it would

be of little or no advantage in reducing the size of the motor in

a power-driven machine, because the lessened thrust would be

counterbalanced by the increased speed per minute. Some years ago

Professor Langley called attention to the great economy of thrust which

might be obtained by using very high speeds, and from this many were led

to suppose that high speed was essential to success in a motor-driven

machine. But the economy to which Professor Langley called attention was

in foot pounds per mile of travel, not in foot pounds per minute. It

is the foot pounds per minute that fixes the size of the motor. The

probability is that the first flying machines will have a relatively low

speed, perhaps not much exceeding 20 miles per hour, but the problem of

increasing the speed will be much simpler in some respects than that of

increasing the speed of a steamboat; for, whereas in the latter case the

size of the engine must increase as the cube of the speed, in the flying

machine, until extremely high speeds are reached, the capacity of the

motor increases in less than simple ratio; and there is even a decrease

in the fuel per mile of travel. In other words, to double the speed of

a steamship (and the same is true of the balloon type of airship) eight

times the engine and boiler capacity would be required, and four times

the fuel consumption per mile of travel: while a flying machine would

require engines of less than double the size, and there would be an

actual decrease in the fuel consumption per mile of travel. But looking

at the matter conversely, the great disadvantage of the flying machine

is apparent; for in the latter no flight at all is possible unless the

proportion of horse-power to flying capacity is very high; but on

the other hand a steamship is a mechanical success if its ratio of

horse-power to tonnage is insignificant. A flying machine that would fly

at a speed of 50 miles per hour with engines of 1,000 horse-power would

not be upheld by its wings at all at a speed of less than 25 miles

an hour, and nothing less than 500 horse-power could drive it at this

speed. But a boat which could make 40 miles an hour with engines of

1,000 horse-power would still move 4 miles an hour even if the engines

were reduced to 1 horse-power. The problems of land and water travel

were solved in the nineteenth century, because it was possible to begin

with small achievements, and gradually work up to our present success.

The flying problem was left over to the twentieth century, because in

this case the art must be highly developed before any flight of any

considerable duration at all can be obtained.

'However, there is another way of flying which requires no artificial

motor, and many workers believe that success will come first by this

road. I refer to the soaring flight, by which the machine is permanently

sustained in the air by the same means that are employed by soaring

birds. They spread their wings to the wind, and sail by the hour,

with no perceptible exertion beyond that required to balance and steer

themselves. What sustains them is not definitely known, though it is

almost certain that it is a rising current of air. But whether it be a

rising current or something else, it is as well able to support a

flying machine as a bird, if man once learns the art of utilising it.

In gliding experiments it has long been known that the rate of vertical

descent is very much retarded, and the duration of the flight greatly

prolonged, if a strong wind blows UP the face of the hill parallel

to its surface. Our machine, when gliding in still air, has a rate of

vertical descent of nearly 6 feet per second, while in a wind blowing

26 miles per hour up a steep hill we made glides in which the rate of

descent was less than 2 feet per second. And during the larger part of

this time, while the machine remained exactly in the rising current,

THERE WAS NO DESCENT AT ALL, BUT EVEN A SLIGHT RISE. If the operator

had had sufficient skill to keep himself from passing beyond the rising

current he would have been sustained indefinitely at a higher point than

that from which he started. The illustration shows one of these very

slow glides at a time when the machine was practically at a standstill.

The failure to advance more rapidly caused the photographer some trouble

in aiming, as you will perceive. In looking at this picture you will

readily understand that the excitement of gliding experiments does

not entirely cease with the breaking up of camp. In the photographic

dark-room at home we pass moments of as thrilling interest as any in

the field, when the image begins to appear on the plate and it is yet an

open question whether we have a picture of a flying machine or merely a

patch of open sky. These slow glides in rising current probably hold out

greater hope of extensive practice than any other method within man's

reach, but they have the disadvantage of requiring rather strong winds

or very large supporting surfaces. However, when gliding operators

have attained greater skill, they can with comparative safety maintain

themselves in the air for hours at a time in this way, and thus by

constant practice so increase their knowledge and skill that they can

rise into the higher air and search out the currents which enable the

soaring birds to transport themselves to any desired point by first

rising in a circle and then sailing off at a descending angle. This

illustration shows the machine, alone, flying in a wind of 35 miles per

hour on the face of a steep hill, 100 feet high. It will be seen

that the machine not only pulls upward, but also pulls forward in the

direction from which the wind blows, thus overcoming both gravity and

the speed of the wind. We tried the same experiment with a man on it,

but found danger that the forward pull would become so strong, that the

men holding the ropes would be dragged from their insecure foothold on

the slope of the hill. So this form of experimenting was discontinued

after four or five minutes' trial.

'In looking over our experiments of the past two years, with models and

full-size machines, the following points stand out with clearness:--

'1. That the lifting power of a large machine, held stationary in a wind

at a small distance from the earth, is much less than the Lilienthal

table and our own laboratory experiments would lead us to expect. When

the machine is moved through the air, as in gliding, the discrepancy

seems much less marked.

'2. That the ratio of drift to lift in well-shaped surfaces is less at

angles of incidence of 5 degrees to 12 degrees than at an angle of 3

degrees.

'3. That in arched surfaces the centre of pressure at 90 degrees is near

the centre of the surface, but moves slowly forward as the angle becomes

less, till a critical angle varying with the shape and depth of the

curve is reached, after which it moves rapidly toward the rear till the

angle of no lift is found.

'4. That with similar conditions large surfaces may be controlled with

not much greater difficulty than small ones, if the control is effected

by manipulation of the surfaces themselves, rather than by a movement of

the body of the operator.

'5. That the head resistances of the framing can be brought to a point

much below that usually estimated as necessary.

'6. That tails, both vertical and horizontal, may with safety be

eliminated in gliding and other flying experiments.

'7. That a horizontal position of the operator's body may be assumed

without excessive danger, and thus the head resistance reduced to about

one-fifth that of the upright position.

'8. That a pair of superposed, or tandem surfaces, has less lift in

proportion to drift than either surface separately, even after making

allowance for weight and head resistance of the connections.'

Thus, to the end of the 1901 experiments, Wilbur Wright provided a

fairly full account of what was accomplished; the record shows an amount

of patient and painstaking work almost beyond belief--it was no question

of making a plane and launching it, but a business of trial and error,

investigation and tabulation of detail, and the rejection time after

time of previously accepted theories, till the brothers must have felt

the the solid earth was no longer secure, at times. Though it was Wilbur

who set down this and other records of the work done, yet the actual

work was so much Orville's as his brother's that no analysis could

separate any set of experiments and say that Orville did this and Wilbur

that--the two were inseparable. On this point Griffith Brewer remarked

that 'in the arguments, if one brother took one view, the other brother

took the opposite view as a matter of course, and the subject was

thrashed to pieces until a mutually acceptable result remained. I have

often been asked since these pioneer days, "Tell me, Brewer, who was

really the originator of those two?" In reply, I used first to say,

"I think it was mostly Wilbur," and later, when I came to know Orville

better, I said, "The thing could not have been without Orville." Now,

when asked, I have to say, "I don't know," and I feel the more I think

of it that it was only the wonderful combination of these two brothers,

who devoted their lives together or this common object, that made the

discovery of the art of flying possible.'

Beyond the 1901 experiments in gliding, the record grows more scrappy,

less detailed. It appears that once power-driven flight had been

achieved, the brothers were not so willing to talk as before;

considering the amount of work that they put in, there could have been

little time for verbal description of that work--as already remarked,

their tables still stand for the designer and experimenter. The end of

the 1901 experiments left both brothers somewhat discouraged, though

they had accomplished more than any others. 'Having set out with

absolute faith in the existing scientific data, we ere driven to doubt

one thing after another, finally, after two years of experiment, we cast

it all aside, and decided to rely entirely on our own investigations.

Truth and error were everywhere so intimately mixed as to be

indistinguishable.... We had taken up aeronautics as a sport. We

reluctantly entered upon the scientific side of it.'

Yet, driven thus to the more serious aspect of the work, they found in

the step its own reward, for the work of itself drew them on and on, to

the construction of measuring machines for the avoidance of error, and

to the making of series after series of measurements, concerning which

Wilbur wrote in 1908 (in the Century Magazine) that 'after making

preliminary measurements on a great number of different shaped surfaces,

to secure a general understanding of the subject, we began systematic

measurements of standard surfaces, so varied in design as to bring

out the underlying causes of differences noted in their pressures.

Measurements were tabulated on nearly fifty of these at all angles from

zero to 45 degrees, at intervals of 2 1/2 degrees. Measurements were

also secured showing the effects on each other when surfaces are

superposed, or when they follow one another.

'Some strange results were obtained. One surface, with a heavy roll at

the front edge, showed the same lift for all angles from 7 1/2 to 45

degrees. This seemed so anomalous that we were almost ready to doubt our

own measurements, when a simple test was suggested. A weather vane, with

two planes attached to the pointer at an angle of 80 degrees with

each other, was made. According to our table, such a vane would be in

unstable equilibrium when pointing directly into the wind, for if by

chance the wind should happen to strike one plane at 39 degrees and the

other at 41 degrees, the plane with the smaller angle would have the

greater pressure and the pointer would be turned still farther out

of the course of the wind until the two vanes again secured equal

pressures, which would be at approximately 30 and 50 degrees. But the

vane performed in this very manner. Further corroboration of the tables

was obtained in experiments with the new glider at Kill Devil Hill the

next season.

'In September and October, 1902 nearly 1,000 gliding flights were made,

several of which covered distances of over 600 feet. Some, made against

a wind of 36 miles an hour, gave proof of the effectiveness of the

devices for control. With this machine, in the autumn of 1903, we made

a number of flights in which we remained in the air for over a minute,

often soaring for a considerable time in one spot, without any descent

at all. Little wonder that our unscientific assistant should think the

only thing needed to keep it indefinitely in the air would be a coat of

feathers to make it light!'

It was at the conclusion of these experiments of 1903 that the brothers

concluded they had obtained sufficient data from their thousands of

glides and multitude of calculations to permit of their constructing

and making trial of a power-driven machine. The first designs got out

provided for a total weight of 600 lbs., which was to include the weight

of the motor and the pilot; but on completion it was found that there

was a surplus of power from the motor, and thus they had 150 lbs. weight

to allow for strengthening wings and other parts.

They came up against the problem to which Riach has since devoted so

much attention, that of propeller design. 'We had thought of getting the

theory of the screw-propeller from the marine engineers, and then, by

applying our table of air-pressures to their formulae, of designing

air-propellers suitable for our uses. But, so far as we could learn, the

marine engineers possessed only empirical formulae, and the exact action

of the screw propeller, after a century of use, was still very obscure.

As we were not in a position to undertake a long series of practical

experiments to discover a propeller suitable for our machine, it seemed

necessary to obtain such a thorough understanding of the theory of its

reactions as would enable us to design them from calculation alone.

What at first seemed a simple problem became more complex the longer we

studied it. With the machine moving forward, the air flying backward,

the propellers turning sidewise, and nothing standing still, it seemed

impossible to find a starting point from which to trace the various

simultaneous reactions. Contemplation of it was confusing. After long

arguments we often found ourselves in the ludicrous position of each

having been converted to the other's side, with no more agreement than

when the discussion began.

'It was not till several months had passed, and every phase of the

problem had been thrashed over and over, that the various reactions

began to untangle themselves. When once a clear understanding had been

obtained there was no difficulty in designing a suitable propeller, with

proper diameter, pitch, and area of blade, to meet the requirements of

the flier. High efficiency in a screw-propeller is not dependent upon

any particular or peculiar shape, and there is no such thing as a "best"

screw. A propeller giving a high dynamic efficiency when used upon one

machine may be almost worthless when used upon another. The propeller

should in every case be designed to meet the particular conditions of

the machine to which it is to be applied. Our first propellers, built

entirely from calculation, gave in useful work 66 per cent of the power

expended. This was about one-third more than had been secured by Maxim

or Langley.'

Langley had made his last attempt with the 'aerodrome,' and his splendid

failure but a few days before the brothers made their first attempt at

power-driven aeroplane flight. On December 17th, 1903, the machine was

taken out; in addition to Wilbur and Orville Wright, there were present

five spectators: Mr A. D. Etheridge, of the Kill Devil life-saving

station; Mr W. S.Dough, Mr W. C. Brinkley, of Manteo; Mr John Ward, of

Naghead, and Mr John T. Daniels.[*] A general invitation had been given

to practically all the residents in the vicinity, but the Kill Devil

district is a cold area in December, and history had recorded so many

experiments in which machines had failed to leave the ground that

between temperature and scepticism only these five risked a waste of

their time.

[*] This list is as given by Wilbur Wright himself.

And these five were in at the greatest conquest man had made since James

Watt evolved the steam engine--perhaps even a greater conquest than that

of Watt. Four flights in all were made; the first lasted only twelve

seconds, 'the first in the history of the world in which a machine

carrying a man had raised itself into the air by its own power in free

flight, had sailed forward on a level course without reduction of

speed, and had finally landed without being wrecked,' said Wilbur

Wright concerning the achievement.[*] The next two flights were slightly

longer, and the fourth and last of the day was one second short of the

complete minute; it was made into the teeth of a 20 mile an hour wind,

and the distance travelled was 852 feet.

[*] Century Magazine, September, 1908.

This bald statement of the day's doings is as Wilbur Wright himself

has given it, and there is in truth nothing more to say; no amount of

statement could add to the importance of the achievement, and no more

than the bare record is necessary. The faith that had inspired the long

roll of pioneers, from da Vinci onward, was justified at last.

Having made their conquest, the brothers took the machine back to camp,

and, as they thought, placed it in safety. Talking with the little group

of spectators about the flights, they forgot about the machine, and then

a sudden gust of wind struck it. Seeing that it was being overturned,

all made a rush toward it to save it, and Mr Daniels, a man of large

proportions, was in some way lifted off his feet, falling between the

planes. The machine overturned fully, and Daniels was shaken like a die

in a cup as the wind rolled the machine over and over--he came out at

the end of his experience with a series of bad bruises, and no more, but

the damage done to the machine by the accident was sufficient to render

it useless for further experiment that season.

A new machine, stronger and heavier, was constructed by the brothers,

and in the spring of 1904 they began experiments again at Sims

Station, eight miles to the east of Dayton, their home town. Press

representatives were invited for the first trial, and about a dozen

came--the whole gathering did not number more than fifty people. 'When

preparations had been concluded,' Wilbur Wright wrote of this trial, 'a

wind of only three or four miles an hour was blowing--insufficient for

starting on so short a track--but since many had come a long way to

see the machine in action, an attempt was made. To add to the other

difficulty, the engine refused to work properly. The machine, after

running the length of the track, slid off the end without rising into

the air at all. Several of the newspaper men returned next day but were

again disappointed. The engine performed badly, and after a glide of

only sixty feet the machine again came to the ground. Further trial was

postponed till the motor could be put in better running condition. The

reporters had now, no doubt, lost confidence in the machine, though

their reports, in kindness, concealed it. Later, when they heard that

we were making flights of several minutes' duration, knowing that longer

flights had been made with airships, and not knowing any essential

difference between airships and flying machines, they were but little

interested.

'We had not been flying long in 1904 before we found that the problem of

equilibrium had not as yet been entirely solved. Sometimes, in making

a circle, the machine would turn over sidewise despite anything the

operator could do, although, under the same conditions in ordinary

straight flight it could have been righted in an instant. In one flight,

in 1905, while circling round a honey locust-tree at a height of about

50 feet, the machine suddenly began to turn up on one wing, and took a

course toward the tree. The operator, not relishing the idea of landing

in a thorn tree, attempted to reach the ground. The left wing, however,

struck the tree at a height of 10 or 12 feet from the ground and carried

away several branches; but the flight, which had already covered a

distance of six miles, was continued to the starting point.

'The causes of these troubles--too technical for explanation here--were

not entirely overcome till the end of September, 1905. The flights then

rapidly increased in length, till experiments were discontinued after

October 5 on account of the number of people attracted to the field.

Although made on a ground open on every side, and bordered on two sides

by much-travelled thoroughfares, with electric cars passing every hour,

and seen by all the people living in the neighbourhood for miles around,

and by several hundred others, yet these flights have been made by some

newspapers the subject of a great "mystery."'

Viewing their work from the financial side, the two brothers incurred

but little expense in the earlier gliding experiments, and, indeed,

viewed these only as recreation, limiting their expenditure to that

which two men might spend on any hobby. When they had once achieved

successful power-driven flight, they saw the possibilities of their

work, and abandoned such other business as had engaged their energies,

sinking all their capital in the development of a practical flying

machine. Having, in 1905, improved their designs to such an extent that

they could consider their machine a practical aeroplane, they devoted

the years 1906 and 1907 to business negotiations and to the construction

of new machines, resuming flying experiments in May of 1908 in order to

test the ability of their machine to meet the requirements of a contract

they had made with the United States Government, which required an

aeroplane capable of carrying two men, together with sufficient fuel

supplies for a flight of 125 miles at 40 miles per hour. Practically

similar to the machine used in the experiments of 1905, the contract

aeroplane was fitted with a larger motor, and provision was made for

seating a passenger and also for allowing of the operator assuming a

sitting position, instead of lying prone.

Before leaving the work of the brothers to consider contemporary events,

it may be noted that they claimed--with justice--that they were first to

construct wings adjustable to different angles of incidence on the right

and left side in order to control the balance of an aeroplane; the

first to attain lateral balance by adjusting wing-tips to respectively

different angles of incidence on the right and left sides, and the first

to use a vertical vane in combination with wing-tips, adjustable to

respectively different angles of incidence, in balancing and steering

an aeroplane. They were first, too, to use a movable vertical tail, in

combination with wings adjustable to different angles of incidence, in

controlling the balance and direction of an aeroplane.[*]

[*]Aeronautical Journal, No. 79.

A certain Henry M. Weaver, who went to see the work of the brothers,

writing in a letter which was subsequently read before the Aero Club de

France records that he had a talk in 1905 with the farmer who rented the

field in which the Wrights made their flights.' On October 5th (1905) he

was cutting corn in the next field east, which is higher ground. When

he noticed the aeroplane had started on its flight he remarked to his

helper: "Well, the boys are at it again," and kept on cutting corn, at

the same time keeping an eye on the great white form rushing about its

course. "I just kept on shocking corn," he continued, "until I got down

to the fence, and the durned thing was still going round. I thought it

would never stop."'

He was right. The brothers started it, and it will never stop.

Mr Weaver also notes briefly the construction of the 1905 Wright flier.

'The frame was made of larch wood-from tip to tip of the wings the

dimension was 40 feet. The gasoline motor--a special construction

made by them--much the same, though, as the motor on the Pope-Toledo

automobile--was of from 12 to 15 horse-power. The motor weighed 240 lbs.

The frame was covered with ordinary muslin of good quality. No attempt

was made to lighten the machine; they simply built it strong enough

to stand the shocks. The structure stood on skids or runners, like a

sleigh. These held the frame high enough from the ground in alighting

to protect the blades of the propeller. Complete with motor, the machine

weighed 925 lbs.

XII. THE FIRST YEARS OF CONQUEST

It is no derogation of the work accomplished by the Wright Brothers to

say that they won the honour of the first power-propelled flights in

a heavier-than-air machine only by a short period. In Europe, and

especially in France, independent experiment was being conducted by

Ferber, by Santos-Dumont, and others, while in England Cody was not far

behind the other giants of those days. The history of the early years

of controlled power flights is a tangle of half-records; there were no

chroniclers, only workers, and much of what was done goes unrecorded

perforce, since it was not set down at the time.

Before passing to survey of those early years, let it be set down that

in 1907, when the Wright Brothers had proved the practicability of their

machines, negotiations were entered into between the brothers and

the British War office. On April 12th 1907, the apostle of military

stagnation, Haldane, then War Minister, put an end to the negotiations

by declaring that 'the War office is not disposed to enter into

relations at present with any manufacturer of aeroplanes' The state

of the British air service in 1914 at the outbreak of hostilities, is

eloquent regarding the pursuance of the policy which Haldane initiated.

'If I talked a lot,' said Wilbur Wright once, 'I should be like the

parrot, which is the bird that speaks most and flies least.' That

attitude is emblematic of the majority of the early fliers, and because

of it the record of their achievements is incomplete to-day. Ferber,

for instance, has left little from which to state what he did, and that

little is scattered through various periodicals, scrappily enough. A

French army officer, Captain Ferber was experimenting with monoplane

and biplane gliders at the beginning of the century-his work was

contemporary with that of the Wrights. He corresponded both with Chanute

and with the Wrights, and in the end he was commissioned by the

French Ministry of War to undertake the journey to America in order

to negotiate with the Wright Brothers concerning French rights in the

patents they had acquired, and to study their work at first hand.

Ferber's experiments in gliding began in 1899 at the Military School at

Fountainebleau, with a canvas glider of some 80 square feet supporting

surface, and weighing 65 lbs. Two years later he constructed a larger

and more satisfactory machine, with which he made numerous excellent

glides. Later, he constructed an apparatus which suspended a plane from

a long arm which swung on a tower, in order that experiments might be

carried out without risk to the experimenter, and it was not until 1905

that he attempted power-driven free flight. He took up the Voisin design

of biplane for his power-driven flights, and virtually devoted all his

energies to the study of aeronautics. His book, Aviation, its Dawn

and Development, is a work of scientific value--unlike many of his

contemporaries, Ferber brought to the study of the problems of flight a

trained mind, and he was concerned equally with the theoretical problems

of aeronautics and the practical aspects of the subject.

After Bleriot's successful cross-Channel flight, it was proposed to

offer a prize of L1,000 for the feat which C. S. Rolls subsequently

accomplished (starting from the English side of the Channel), a flight

from Boulogne to Dover and back; in place of this, however, an aviation

week at Boulogne was organised, but, although numerous aviators were

invited to compete, the condition of the flying grounds was such that

no competitions took place. Ferber was virtually the only one to do any

flying at Boulogne, and at the outset he had his first accident; after

what was for those days a good flight, he made a series of circles

with his machine, when it suddenly struck the ground, being partially

wrecked. Repairs were carried out, and Ferber resumed his exhibition

flights, carrying on up to Wednesday, September 22nd, 1909. On that day

he remained in the air for half an hour, and, as he was about to land,

the machine struck a mound of earth and overturned, pinning Ferber under

the weight of the motor. After being extricated, Ferber seemed to show

little concern at the accident, but in a few minutes he complained of

great pain, when he was conveyed to the ambulance shed on the ground.

'I was foolish,' he told those who were with him there. 'I was flying

too low. It was my own fault and it will be a severe lesson to me.

I wanted to turn round, and was only five metres from the ground.' A

little after this, he got up from the couch on which he had been placed,

and almost immediately collapsed, dying five minutes later.

Ferber's chief contemporaries in France were Santos-Dumont, of airship

fame, Henri and Maurice Farman, Hubert Latham, Ernest Archdeacon, and

Delagrange. These are names that come at once to mind, as does that of

Bleriot, who accomplished the second great feat of power-driven flight,

but as a matter of fact the years 1903-10 are filled with a little host

of investigators and experimenters, many of whom, although their names

do not survive to any extent, are but a very little way behind those

mentioned here in enthusiasm and devotion. Archdeacon and Gabriel

Voisin, the former of whom took to heart the success achieved by the

Wright Brothers, co-operated in experiments in gliding. Archdeacon

constructed a glider in box-kite fashion, and Voisin experimented with

it on the Seine, the glider being towed by a motorboat to attain the

necessary speed. It was Archdeacon who offered a cup for the first

straight flight of 200 metres, which was won by Santos-Dumont, and he

also combined with Henri Deutsch de la Meurthe in giving the prize for

the first circular flight of a mile, which was won by Henry Farman on

January 13th, 1908.

A history of the development of aviation in France in these, the

strenuous years, would fill volumes in itself. Bleriot was carrying

out experiments with a biplane glider on the Seine, and Robert

Esnault-Pelterie was working on the lines of the Wright Brothers,

bringing American practice to France. In America others besides the

Wrights had wakened to the possibilities of heavier-than-air flight;

Glenn Curtiss, in company with Dr Alexander Graham Bell, with J. A. D.

McCurdy, and with F. W. Baldwin, a Canadian engineer, formed the Aerial

Experiment Company, which built a number of aeroplanes, most famous of

which were the 'June Bug,' the 'Red Wing,' and the 'White Wing.' In 1908

the 'June Bug 'won a cup presented by the Scientific American--it was

the first prize offered in America in connection with aeroplane flight.

Among the little group of French experimenters in these first years of

practical flight, Santos-Dumont takes high rank. He built his 'No. 14

bis' aeroplane in biplane form, with two superposed main plane surfaces,

and fitted it with an eight-cylinder Antoinette motor driving a

two-bladed aluminium propeller, of which the blades were 6 feet only

from tip to tip. The total lift surface of 860 square feet was given

with a wing-span of a little under 40 feet, and the weight of the

complete machine was 353 lbs., of which the engine weighed 158 lbs.

In July of 1906 Santos-Dumont flew a distance of a few yards in this

machine, but damaged it in striking the ground; on October 23rd of the

same year he made a flight of nearly 200 feet--which might have been

longer, but that he feared a crowd in front of the aeroplane and cut

off his ignition. This may be regarded as the first effective flight in

Europe, and by it Santos-Dumont takes his place as one of the chief--if

not the chief--of the pioneers of the first years of practical flight,

so far as Europe is concerned.

Meanwhile, the Voisin Brothers, who in 1904 made cellular kites for

Archdeacon to test by towing on the Seine from a motor launch, obtained

data for the construction of the aeroplane which Delagrange and Henry

Farman were to use later. The Voisin was a biplane, constructed with

due regard to the designs of Langley, Lilienthal, and other earlier

experimenters--both the Voisins and M. Colliex, their engineer, studied

Lilienthal pretty exhaustively in getting out their design, though their

own researches were very thorough as well. The weight of this Voisin

biplane was about 1,450 lbs., and its maximum speed was some 38 to 40

miles per hour, the total supporting surface being about 535 square

feet. It differed from the Wright design in the possession of a

tail-piece, a characteristic which marked all the French school of early

design as in opposition to the American. The Wright machine got its

longitudinal stability by means of the main planes and the elevating

planes, while the Voisin type added a third factor of stability in its

sailplanes. Further, the Voisins fitted their biplane with a wheeled

undercarriage, while the Wright machine, being fitted only with runners,

demanded a launching rail for starting. Whether a machine should be

tailless or tailed was for some long time matter for acute controversy,

which in the end was settled by the fitting of a tail to the Wright

machines-France won the dispute by the concession.

Henry Farman, who began his flying career with a Voisin machine, evolved

from it the aeroplane which bore his name, following the main lines of

the Voisin type fairly closely, but making alterations in the controls,

and in the design of the undercarriage, which was somewhat elaborated,

even to the inclusion of shock absorbers. The seven-cylinder 50

horse-power Gnome rotary engine was fitted to the Farman machine--the

Voisins had fitted an eight-cylinder Antoinette, giving 50 horse-power

at 1,100 revolutions per minute, with direct drive to the propeller.

Farman reduced the weight of the machine from the 1,450 lbs. of the

Voisins to some 1,010 lbs. or thereabouts, and the supporting area to

450 square feet. This machine won its chief fame with Paulhan as pilot

in the famous London to Manchester flight--it is to be remarked, too,

that Farman himself was the first man in Europe to accomplish a flight

of a mile.

Other notable designs of these early days were the 'R.E.P.', Esnault

Pelterie's machine, and the Curtiss-Herring biplane. Of these Esnault

Pelterie's was a monoplane, designed in that form since Esnault Pelterie

had found by experiment that the wire used in bracing offers far more

resistance to the air than its dimensions would seem to warrant. He

built the wings of sufficient strength to stand the strain of flight

without bracing wires, and dependent only for their support on the

points of attachment to the body of the machine; for the rest, it

carried its propeller in front of the planes, and both horizontal and

vertical rudders at the stern--a distinct departure from the Wright

and similar types. One wheel only was fixed under the body where the

undercarriage exists on a normal design, but light wheels were fixed,

one at the extremity of each wing, and there was also a wheel under the

tail portion of the machine. A single lever actuated all the controls

for steering. With a supporting surface of 150 square feet the machine

weighed 946 lbs., about 6.4 lbs. per square foot of lifting surface.

The Curtiss biplane, as flown by Glenn Curtiss at the Rheims meeting,

was built with a bamboo framework, stayed by means of very fine

steel-stranded cables. A--then--novel feature of the machine was the

moving of the ailerons by the pilot leaning to one side or the other in

his seat, a light, tubular arm-rest being pressed by his body when he

leaned to one side or the other, and thus operating the movement of the

ailerons employed for tilting the plane when turning. A steering-wheel

fitted immediately in front of the pilot's seat served to operate a rear

steering-rudder when the wheel was turned in either direction, while

pulling back the wheel altered the inclination of the front elevating

planes, and so gave lifting or depressing control of the plane.

This machine ran on three wheels before leaving the ground, a central

undercarriage wheel being fitted in front, with two more in line with

a right angle line drawn through the centre of the engine crank at the

rear end of the crank-case. The engine was a 35 horsepower Vee design,

water cooled, with overhead inlet and exhaust valves, and Bosch

high-tension magneto ignition. The total weight of the plane in flying

order was about 700 lbs.

As great a figure in the early days as either Ferber or Santos-Dumont

was Louis Bleriot, who, as early as 1900 built a flapping-wing model,

this before ever he came to experimenting with the Voisin biplane type

of glider on the Seine. Up to 1906 he had built four biplanes of his own

design, and in March of 1907 he built his first monoplane, to wreck

it only a few days after completion in an accident from which he had

a fortunate escape. His next machine was a double monoplane, designed

after Langley's precept, to a certain extent, and this was totally

wrecked in September of 1907. His seventh machine, a monoplane, was

built within a month of this accident, and with this he had a number

of mishaps, also achieving some good flights, including one in which

he made a turn. It was wrecked in December of 1907, whereupon he built

another monoplane on which, on July 6th, 1908, Bleriot made a flight

lasting eight and a half minutes. In October of that year he flew the

machine from Toury to Artenay and returned on it--this was just a day

after Farman's first cross-country flight--but, trying to repeat the

success five days later, Bleriot collided with a tree in a fog and

wrecked the machine past repair. Thereupon he set about building his

eleventh machine, with which he was to achieve the first flight across

the English channel.

Henry Farman, to whom reference has already been made, was engaged with

his two brothers, Maurice and Richard, in the motor-car business, and

turned to active interest in flying in 1907, when the Voisin firm built

his first biplane on the box-kite principle. In July of 1908 he won

a prize of L400 for a flight of thirteen miles, previously having

completed the first kilometre flown in Europe with a passenger, the said

passenger being Ernest Archdeaon. In September of 1908 Farman put up a

speed record of forty miles an hour in a flight lasting forty minutes.

Santos-Dumont produced the famous 'Demoiselle' monoplane early in 1909,

a tiny machine in which the pilot had his seat in a sort of miniature

cage under the main plane. It was a very fast, light little machine but

was difficult to fly, and owing to its small wingspread was unable

to glide at a reasonably safe angle. There has probably never been a

cheaper flying machine to build than the 'Demoiselle,' which could be so

upset as to seem completely wrecked, and then repaired ready for further

flight by a couple of hours' work. Santos-Dumont retained no patent

in the design, but gave it out freely to any one who chose to build

'Demoiselles'; the vogue of the pattern was brief, owing to the

difficulty of piloting the machine.

These were the years of records, broken almost as soon as made. There

was Farman's mile, there was the flight of the Comte de Lambert over the

Eiffel Tower, Latham's flight at Blackpool in a high wind, the Rheims

records, and then Henry Farman's flight of four hours later in 1909,

Orville Wright's height record of 1,640 feet, and Delagrange's speed

record of 49.9 miles per hour. The coming to fame of the Gnome rotary

engine helped in the making of these records to a very great extent,

for in this engine was a prime mover which gave the reliability that

aeroplane builders and pilots had been searching for, but vainly. The

Wrights and Glenn Curtiss, of course, had their own designs of engine,

but the Gnome, in spite of its lack of economy in fuel and oil, and its

high cost, soon came to be regarded as the best power plant for flight.

Delagrange, one of the very good pilots of the early days, provided a

curious insight to the way in which flying was regarded, at the opening

of the Juvisy aero aerodrome in May of 1909. A huge crowd had gathered

for the first day's flying, and nine machines were announced to appear,

but only three were brought out. Delagrange made what was considered an

indifferent little flight, and another pilot, one De Bischoff, attempted

to rise, but could not get his machine off the ground. Thereupon the

crowd of 30,000 people lost their tempers, broke down the barriers

surrounding the flying course, and hissed the officials, who were quite

unable to maintain order. Delagrange, however, saved the situation

by making a circuit of the course at a height of thirty feet from the

ground, which won him rounds of cheering and restored the crowd to

good humour. Possibly the smash achieved by Rougier, the famous racing

motorist, who crashed his Voisin biplane after Delagrange had made his

circuit, completed the enjoyment of the spectators. Delagrange, flying

at Argentan in June of 1909, made a flight of four kilometres at a

height of sixty feet; for those days this was a noteworthy performance.

Contemporary with this was Hubert Latham's flight of an hour and seven

minutes on an Antoinette monoplane; this won the adjective 'magnificent'

from contemporary recorders of aviation.

Viewing the work of the little group of French experimenters, it is,

at this length of time from their exploits, difficult to see why

they carried the art as far as they did. There was in it little of

satisfaction, a certain measure of fame, and practically no profit--the

giants of those days got very little for their pains. Delagrange's

experience at the opening of the Juvisy ground was symptomatic of the

way in which flight was regarded by the great mass of people--it was a

sport, and nothing more, but a sport without the dividends attaching

to professional football or horse-racing. For a brief period, after the

Rheims meeting, there was a golden harvest to be reaped by the best of

the pilots. Henry Farman asked L2,000 for a week's exhibition flying in

England, and Paulhan asked half that sum, but a rapid increase in

the number of capable pilots, together with the fact that most flying

meetings were financial failures, owing to great expense in organisation

and the doubtful factor of the weather, killed this goose before many

golden eggs had been gathered in by the star aviators. Besides, as

height and distance records were broken one after another, it became

less and less necessary to pay for entrance to an aerodrome in order to

see a flight--the thing grew too big for a mere sports ground.

Long before Rheims and the meeting there, aviation had grown too big for

the chronicling of every individual effort. In that period of the first

days of conquest of the air, so much was done by so many whose names

are now half-forgotten that it is possible only to pick out the great

figures and make brief reference to their achievements and the machines

with which they accomplished so much, pausing to note such epoch-making

events as the London-Manchester flight, Bleriot's Channel crossing,

and the Rheims meeting itself, and then passing on beyond the days of

individual records to the time when the machine began to dominate the

man. This latter because, in the early days, it was heroism to trust

life to the planes that were turned out--the 'Demoiselle' and the

Antoinette machine that Latham used in his attempt to fly the Channel

are good examples of the flimsiness of early types--while in the later

period, that of the war and subsequently, the heroism turned itself in a

different--and nobler-direction. Design became standardised, though

not perfected. The domination of the machine may best be expressed by

contrasting the way in which machines came to be regarded as compared

with the men who flew them: up to 1909, flying enthusiasts talked of

Farman, of Bleriot, of Paulhan, Curtiss, and of other men; later, they

began to talk of the Voisin, the Deperdussin, and even to the Fokker,

the Avro, and the Bristol type. With the standardising of the machine,

the days of the giants came to an end.

XIII. FIRST FLIERS IN ENGLAND

Certain experiments made in England by Mr Phillips seem to have come

near robbing the Wright Brothers of the honour of the first flight;

notes made by Colonel J. D. Fullerton on the Phillips flying machine

show that in 1893 the first machine was built with a length of 25 feet,

breadth of 22 feet, and height of 11 feet, the total weight, including a

72 lb. load, being 420 lbs. The machine was fitted with some fifty wood

slats, in place of the single supporting surface of the monoplane or two

superposed surfaces of the biplane, these slats being fixed in a steel

frame so that the whole machine rather resembled a Venetian blind. A

steam engine giving about 9 horse-power provided the motive power for

the six-foot diameter propeller which drove the machine. As it was

not possible to put a passenger in control as pilot, the machine was

attached to a central post by wire guys and run round a circle 100

feet in diameter, the track consisting of wooden planking 4 feet wide.

Pressure of air under the slats caused the machine to rise some two or

three feet above the track when sufficient velocity had been attained,

and the best trials were made on June 19th 1893, when at a speed of 40

miles an hour, with a total load of 385 lbs., all the wheels were off

the ground for a distance of 2,000 feet.

In 1904 a full-sized machine was constructed by Mr Phillips, with a

total weight, including that of the pilot, of 600 lbs. The machine was

designed to lift when it had attained a velocity of 50 feet per

second, the motor fitted giving 22 horse-power. On trial, however, the

longitudinal equilibrium was found to be defective, and a further design

was got out, the third machine being completed in 1907. In this the wood

slats were held in four parallel container frames, the weight of the

machine, excluding the pilot, being 500 lbs. A motor similar to that

used in the 1904 machine was fitted, and the machine was designed to

lift at a velocity of about 30 miles an hour, a seven-foot propeller

doing the driving. Mr Phillips tried out this machine in a field about

400 yards across. 'The machine was started close to the hedge, and rose

from the ground when about 200 yards had been covered. When the machine

touched the ground again, about which there could be no doubt, owing to

the terrific jolting, it did not run many yards. When it came to rest I

was about ten yards from the boundary. Of course, I stopped the engine

before I commenced to descend.'[*]

[*] Aeronautical Journal, July, 1908.

S. F. Cody, an American by birth, aroused the attention not only of the

British public, but of the War office and Admiralty as well, as early as

1905 with his man-lifting kites. In that year a height of 1,600 feet was

reached by one of these box-kites, carrying a man, and later in the same

year one Sapper Moreton, of the Balloon Section of the Royal Engineers

(the parent of the Royal Flying Corps) remained for an hour at an

altitude of 2,600 feet. Following on the success of these kites, Cody

constructed an aeroplane which he designated a 'power kite,' which

was in reality a biplane that made the first flight in Great Britain.

Speaking before the Aeronautical Society in 1908, Cody said that 'I have

accomplished one thing that I hoped for very much, that is, to be the

first man to fly in Great Britain.... I made a machine that left the

ground the first time out; not high, possibly five or six inches only. I

might have gone higher if I wished. I made some five flights in all, and

the last flight came to grief.... On the morning of the accident I

went out after adjusting my propellers at 8 feet pitch running at 600

(revolutions per minute). I think that I flew at about twenty-eight

miles per hour. I had 50 horsepower motor power in the engine. A bunch

of trees, a flat common above these trees, and from this flat there is a

slope goes down... to another clump of trees. Now, these clumps of trees

are a quarter of a mile apart or thereabouts.... I was accused of doing

nothing but jumping with my machine, so I got a bit agitated and went to

fly.

I went out this morning with an easterly wind, and left the ground at

the bottom of the hill and struck the ground at the top, a distance of

74 yards. That proved beyond a doubt that the machine would fly--it

flew uphill. That was the most talented flight the machine did, in my

opinion. Now, I turned round at the top and started the machine and left

the ground--remember, a ten mile wind was blowing at the time. Then, 60

yards from where the men let go, the machine went off in this direction

(demonstrating)--I make a line now where I hoped to land--to cut these

trees off at that side and land right off in here. I got here somewhat

excited, and started down and saw these trees right in front of me. I

did not want to smash my head rudder to pieces, so I raised it again and

went up. I got one wing direct over that clump of trees, the right wing

over the trees, the left wing free; the wind, blowing with me, had to

lift over these trees. So I consequently got a false lift on the right

side and no lift on the left side. Being only about 8 feet from the

tree tops, that turned my machine up like that (demonstrating). This

end struck the ground shortly after I had passed the trees. I pulled the

steering handle over as far as I could. Then I faced another bunch of

trees right in front of me. Trying to avoid this second bunch of trees I

turned the rudder, and turned it rather sharp. That side of the machine

struck, and it crumpled up like so much tissue paper, and the machine

spun round and struck the ground that way on, and the framework was

considerably wrecked. Now, I want to advise all aviators not to try

to fly with the wind and to cross over any big clump of earth or any

obstacle of any description unless they go square over the top of it,

because the lift is enormous crossing over anything like that, and in

coming the other way against the wind it would be the same thing when

you arrive at the windward side of the obstacle. That is a point I did

not think of, and had I thought of it I would have been more cautious.'

This Cody machine was a biplane with about 40 foot span, the wings being

about 7 feet in depth with about 8 feet between upper and lower wing

surfaces. 'Attached to the extremities of the lower planes are two small

horizontal planes or rudders, while a third small vertical plane is

fixed over the centre of the upper plane.' The tail-piece and principal

rudder were fitted behind the main body of the machine, and a horizontal

rudder plane was rigged out in front, on two supporting arms extending

from the centre of the machine. The small end-planes and the vertical

plane were used in conjunction with the main rudder when turning to

right or left, the inner plane being depressed on the turn, and the

outer one correspondingly raised, while the vertical plane, working in

conjunction, assisted in preserving stability. Two two-bladed propellers

were driven by an eight-cylinder 50 horse-power Antoinette motor. With

this machine Cody made his first flights over Laffan's plain, being then

definitely attached to the Balloon Section of the Royal Engineers as

military aviation specialist.

There were many months of experiment and trial, after the accident which

Cody detailed in the statement given above, and then, on May 14th, 1909,

Cody took the air and made a flight of 1,200 yards with entire success.

Meanwhile A. V. Roe was experimenting at Lea Marshes with a triplane

of rather curious design the pilot having his seat between two sets of

three superposed planes, of which the front planes could be tilted and

twisted while the machine was in motion. He comes but a little way after

Cody in the chronology of early British experimenters, but Cody, a born

inventor, must be regarded as the pioneer of the present century so

far as Britain is concerned. He was neither engineer nor trained

mathematician, but he was a good rule-of-thumb mechanic and a man of

pluck and perseverance; he never strove to fly on an imperfect machine,

but made alteration after alteration in order to find out what was

improvement and what was not, in consequence of which it was said of him

that he was 'always satisfied with his alterations.'

By July of 1909 he had fitted an 80 horse-power motor to his biplane,

and with this he made a flight of over four miles over Laffan's Plain on

July 21st. By August he was carrying passengers, the first being Colonel

Capper of the R.E. Balloon Section, who flew with Cody for over

two miles, and on September 8th, 1909, he made a world's record

cross-country flight of over forty miles in sixty-six minutes, taking

a course from Laffan's Plain over Farnborough, Rushmoor, and Fleet,

and back to Laffan's Plain. He was one of the competitors in the 1909

Doncaster Aviation Meeting, and in 1910 he competed at Wolverhampton,

Bournemouth, and Lanark. It was on June 7th, 1910, that he qualified for

his brevet, No. 9, on the Cody biplane.

He built a machine which embodied all the improvements for which he had

gained experience, in 1911, a biplane with a length of 35 feet and

span of 43 feet, known as the 'Cody cathedral' on account of its

rather cumbrous appearance. With this, in 1911, he won the two Michelin

trophies presented in England, completed the Daily Mail circuit of

Britain, won the Michelin cross-country prize in 1912 and altogether, by

the end of 1912, had covered more than 7,000 miles with the machine.

It was fitted with a 120 horse-power Austro-Daimler engine, and was

characterised by an exceptionally wide range of speed--the great

wingspread gave a slow landing speed.

A few of his records may be given: in 1910, flying at Laffan's Plain in

his biplane, fitted with a 50-60 horsepower Green engine, on December

31st, he broke the records for distance and time by flying 185 miles,

787 yards, in 4 hours 37 minutes. On October 31st, 1911, he beat this

record by flying for 5 hours 15 minutes, in which period he covered

261 miles 810 yards with a 60 horse-power Green engine fitted to his

biplane. In 1912, competing in the British War office tests of military

aeroplanes, he won the L5,000 offered by the War Office. This was in

competition with no less than twenty-five other machines, among which

were the since-famous Deperdussin, Bristol, Flanders, and Avro types,

as well as the Maurice Farman and Bleriot makes of machine. Cody's

remarkable speed range was demonstrated in these trials, the speeds of

his machine varying between 72.4 and 48.5 miles per hour. The machine

was the only one delivered for the trials by air, and during the three

hours' test imposed on all competitors a maximum height of 5,000 feet

was reached, the first thousand feet being achieved in three and a half

minutes.

During the summer of 1913 Cody put his energies into the production of

a large hydro-biplane, with which he intended to win the L5,000 prize

offered by the Daily Mail to the first aviator to fly round Britain on

a waterplane. This machine was fitted with landing gear for its tests,

and, while flying it over Laffan's Plain on August 7th, 1913, with Mr W.

H. B. Evans as passenger, Cody met with the accident that cost both

him and his passenger their lives. Aviation lost a great figure by his

death, for his plodding, experimenting, and dogged courage not only won

him the fame that came to a few of the pilots of those days, but also

advanced the cause of flying very considerably and contributed not a

little to the sum of knowledge in regard to design and construction.

Another figure of the early days was A. V. Roe, who came from marine

engineering to the motor industry and aviation in 1905. In 1906 he went

out to Colorado, getting out drawings for the Davidson helicopter, and

in 1907 having returned to England, he obtained highest award out of 200

entries in a model aeroplane flying competition. From the design of

this model he built a full-sized machine, and made a first flight on it,

fitted with a 24 horse-power Antoinette engine, in June of 1908 Later,

he fitted a 9 horsepower motor-cycle engine to a triplane of his own

design, and with this made a number of short flights; he got his flying

brevet on a triplane with a motor of 35 horse-power, which, together

with a second triplane, was entered for the Blackpool aviation meeting

of 1910 but was burnt in transport to the meeting. He was responsible

for the building of the first seaplane to rise from English waters, and

may be counted the pioneer of the tractor type of biplane. In 1913 he

built a two-seater tractor biplane with 80 horse-power engine, a machine

which for some considerable time ranked as a leader of design. Together

with E. V. Roe and H. V. Roe, 'A. V.' controlled the Avro works, which

produced some of the most famous training machines of the war period in

a modification of the original 80 horse-power tractor. The first of the

series of Avro tractors to be adopted by the military authorities was

the 1912 biplane, a two-seater fitted with 50 horsepower engine. It was

the first tractor biplane with a closed fuselage to be used for military

work, and became standard for the type. The Avro seaplane, of I 100

horse-power (a fourteen-cylinder Gnome engine was used) was taken up

by the British Admiralty in 1913. It had a length of 34 feet and a

wing-span of 50 feet, and was of the twin-float type.

Geoffrey de Havilland, though of later rank, counts high among designers

of British machines. He qualified for his brevet as late as February,

1911, on a biplane of his own construction, and became responsible for

the design of the BE2, the first successful British Government biplane.

On this he made a British height record of 10,500 feet over Salisbury

Plain, in August of 1912, when he took up Major Sykes as passenger. In

the war period he was one of the principal designers of fighting and

reconnaissance machines.

F. Handley Page, who started in business as an aeroplane builder in

1908, having works at Barking, was one of the principal exponents of

the inherently stable machine, to which he devoted practically all his

experimental work up to the outbreak of war. The experiments were made

with various machines, both of monoplane and biplane type, and of these

one of the best was a two-seater monoplane built in 1911, while a second

was a larger machine, a biplane, built in 1913 and fitted with a 110

horse-power Anzani engine. The war period brought out the giant biplane

with which the name of Handley Page is most associated, the twin-engined

night-bomber being a familiar feature of the later days of the war;

the four-engined bomber had hardly had a chance of proving itself under

service conditions when the war came to an end.

Another notable figure of the early period was 'Tommy' Sopwith, who took

his flying brevet at Brooklands in November of 1910, and within four

days made the British duration record of 108 miles in 3 hours 12

minutes. On December 18th, 1910, he won the Baron de Forrest prize of

L4,000 for the longest flight from England to the Continent, flying

from Eastchurch to Tirlemont, Belgium, in three hours, a distance of 161

miles. After two years of touring in America, he returned to England and

established a flying school. In 1912 he won the first aerial Derby, and

in 1913 a machine of his design, a tractor biplane, raised the British

height record to 13,000 feet (June 16th, at Brooklands). First as

aviator, and then as designer, Sopwith has done much useful work in

aviation.

These are but a few, out of a host who contributed to the development of

flying in this country, for, although France may be said to have set

the pace as regards development, Britain was not far behind. French

experimenters received far more Government aid than did the early

British aviators and designers--in the early days the two were

practically synonymous, and there are many stories of the very early

days at Brooklands, where, when funds ran low, the ardent spirits

patched their trousers with aeroplane fabric and went on with their work

with Bohemian cheeriness. Cody, altering and experimenting on Laffan's

Plain, is the greatest figure of them all, but others rank, too, as

giants of the early days, before the war brought full recognition of the

aeroplane's potentialities.

One of the first men actually to fly in England, Mr J. C. T.

Moore-Brabazon, was a famous figure in the days of exhibition flying,

and won his reputation mainly through being first to fly a circular

mile on a machine designed and built in Great Britain and piloted by a

British subject. Moore-Brabazon's earliest flights were made in France

on a Voisin biplane in 1908, and he brought this machine over to

England, to the Aero Club grounds at Shellness, but soon decided that he

would pilot a British machine instead. An order was placed for a Short

machine, and this, fitted with a 50-60 horse-power Green engine, was

used for the circular mile, which won a prize of L1,000 offered by the

Daily Mail, the feat being accomplished on October 30th, 1909. Five

days later, Moore-Brabazon achieved the longest flight up to that time

accomplished on a British-built machine, covering three and a half

miles. In connection with early flying in England, it is claimed that A.

V. Roe, flying 'Avro B,',' on June 8th, 1908, was actually the first man

to leave the ground, this being at Brooklands, but in point of fact Cody

antedated him.

No record of early British fliers could be made without the name of C.

S. Rolls, a son of Lord Llangattock, on June 2nd, 1910, he flew across

the English Channel to France, until he was duly observed over French

territory, when he returned to England without alighting. The trip was

made on a Wright biplane, and was the third Channel crossing by air,

Bleriot having made the first, and Jacques de Lesseps the second. Rolls

was first to make the return journey in one trip. He was eventually

killed through the breaking of the tail-plane of his machine in

descending at a flying meeting at Bournemouth. The machine was a Wright

biplane, but the design of the tail-plane--which, by the way, was

an addition to the machine, and was not even sanctioned by the

Wrights--appears to have been carelessly executed, and the plane itself

was faulty in construction. The breakage caused the machine to overturn,

killing Rolls, who was piloting it.

XIV. RHEIMS, AND AFTER

The foregoing brief--and necessarily incomplete--survey of the early

British group of fliers has taken us far beyond some of the great events

of the early days of successful flight, and it is necessary to go back

to certain landmarks in the history of aviation, first of which is the

great meeting at Rheims in 1909. Wilbur Wright had come to Europe,

and, flying at Le Mans and Pau--it was on August 8th, 1908, that Wilbur

Wright made the first of his ascents in Europe--had stimulated public

interest in flying in France to a very great degree. Meanwhile, Orville

Wright, flying at Fort Meyer, U.S.A., with Lieutenant Selfridge as a

passenger, sustained an accident which very nearly cost him his life

through the transmission gear of the motor breaking. Selfridge was

killed and Orville Wright was severely injured--it was the first fatal

accident with a Wright machine.

Orville Wright made a flight of over an hour on September 9th, 1908, and

on December 31st of that year Wilbur flew for 2 hours 19 minutes. Thus,

when the Rheims meeting was organised--more notable because it was the

first of its kind, there were already records waiting to be broken. The

great week opened on August 22nd, there being thirty entrants, including

all the most famous men among the early fliers in France. Bleriot,

fresh from his Channel conquest, was there, together with Henry Farman,

Paulhan, Curtiss, Latham, and the Comte de Lambert, first pupil of the

Wright machine in Europe to achieve a reputation as an aviator.

'To say that this week marks an epoch in the history of the world is to

state a platitude. Nevertheless, it is worth stating, and for us who

are lucky enough to be at Rheims during this week there is a solid

satisfaction in the idea that we are present at the making of history.

In perhaps only a few years to come the competitions of this week may

look pathetically small and the distances and speeds may appear paltry.

Nevertheless, they are the first of their kind, and that is sufficient.'

So wrote a newspaper correspondent who was present at the famous

meeting, and his words may stand, being more than mere journalism; for

the great flying week which opened on August 22nd, 1909, ranks as one of

the great landmarks in the history of heavier-than-air flight. The day

before the opening of the meeting a downpour of rain spoilt the flying

ground; Sunday opened with a fairly high wind, and in a lull M.

Guffroy turned out on a crimson R.E.P. monoplane, but the wheels of

his undercarriage stuck in the mud and prevented him from rising in

the quarter of an hour allowed to competitors to get off the ground.

Bleriot, following, succeeded in covering one side of the triangular

course, but then came down through grit in the carburettor. Latham,

following him with thirteen as the number of his machine, experienced

his usual bad luck and came to earth through engine trouble after a very

short flight. Captain Ferber, who, owing to military regulations, always

flew under the name of De Rue, came out next with his Voisin biplane,

but failed to get off the ground; he was followed by Lefebvre on a

Wright biplane, who achieved the success of the morning by rounding the

course--a distance of six and a quarter miles--in nine minutes with a

twenty mile an hour wind blowing. His flight finished the morning.

Wind and rain kept competitors out of the air until the evening, when

Latham went up, to be followed almost immediately by the Comte de

Lambert. Sommer, Cockburn (the only English competitor), Delagrange,

Fournier, Lefebvre, Bleriot, Bunau-Varilla, Tissandier, Paulhan,

and Ferber turned out after the first two, and the excitement of the

spectators at seeing so many machines in the air at one time provoked

wild cheering. The only accident of the day came when Bleriot damaged

his propeller in colliding with a haycock.

The main results of the day were that the Comte de Lambert flew 30

kilometres in 29 minutes 2 seconds; Lefebvre made the ten-kilometre

circle of the track in just a second under 9 minutes, while Tissandier

did it in 9 1/4 minutes, and Paulhan reached a height of 230 feet. Small

as these results seem to us now, and ridiculous as may seem enthusiasm

at the sight of a few machines in the air at the same time, the Rheims

Meeting remains a great event, since it proved definitely to the whole

world that the conquest of the air had been achieved.

Throughout the week record after record was made and broken. Thus on

the Monday, Lefebvre put up a record for rounding the course and Bleriot

beat it, to be beaten in turn by Glenn Curtiss on his Curtiss-Herring

biplane. On that day, too, Paulhan covered 34 3/4 miles in 1 hour 6

minutes. On the next day, Paulhan on his Voisin biplane took the air

with Latham, and Fournier followed, only to smash up his machine by

striking an eddy of wind which turned him over several times. On the

Thursday, one of the chief events was Latham's 43 miles accomplished in

1 hour 2 minutes in the morning and his 96.5 miles in 2 hours 13 minutes

in the afternoon, the latter flight only terminated by running out of

petrol. On the Friday, the Colonel Renard French airship, which had

flown over the ground under the pilotage of M. Kapfarer, paid Rheims a

second visit; Latham manoeuvred round the airship on his Antoinette and

finally left it far behind. Henry Farman won the Grand Prix de Champagne

on this day, covering 112 miles in 3 hours, 4 minutes, 56 seconds,

Latham being second with his 96.5 miles flight, and Paulhan third.

On the Saturday, Glenn Curtiss came to his own, winning the

Gordon-Bennett Cup by covering 20 kilometres in 15 minutes 50.6 seconds.

Bleriot made a good second with 15 minutes 56.2 seconds as his time,

and Latham and Lefebvre were third and fourth. Farman carried off the

passenger prize by carrying two passengers a distance of 6 miles in 10

minutes 39 seconds. On the last day Delagrange narrowly escaped serious

accident through the bursting of his propeller while in the air, Curtiss

made a new speed record by travelling at the rate of over 50 miles an

hour, and Latham, rising to 500 feet, won the altitude prize.

These are the cold statistics of the meeting; at this length of time it

is difficult to convey any idea of the enthusiasm of the crowds over

the achievements of the various competitors, while the incidents of

the week, comic and otherwise, are nearly forgotten now even by those

present in this making of history. Latham's great flight on the Thursday

was rendered a breathless episode by a downpour of rain when he had

covered all but a kilometre of the record distance previously achieved

by Paulhan, and there was wild enthusiasm when Latham flew on through

the rain until he had put up a new record and his petrol had run out.

Again, on the Friday afternoon, the Colonel Renard took the air together

with a little French dirigible, Zodiac III; Latham was already in the

air directly over Farman, who was also flying, and three crows which

turned out as rivals to the human aviators received as much cheering for

their appearance as had been accorded to the machines, which doubtless

they could not understand. Frightened by the cheering, the crows tried

to escape from the course, but as they came near the stands, the crowd

rose to cheer again and the crows wheeled away to make a second charge

towards safety, with the same result; the crowd rose and cheered at them

a third and fourth time; between ten and fifteen thousand people stood

on chairs and tables and waved hats and handkerchiefs at three ordinary,

everyday crows. One thoughtful spectator, having thoroughly enjoyed the

funny side of the incident, remarked that the ultimate mastery of the

air lies with the machine that comes nearest to natural flight. This

still remains for the future to settle.

Farman's world record, which won the Grand Prix de Champagne, was done

with a Gnome Rotary Motor which had only been run on the test bench

and was fitted to his machine four hours before he started on the great

flight. His propeller had never been tested, having only been completed

the night before. The closing laps of that flight, extending as they did

into the growing of the dusk, made a breathlessly eerie experience for

such of the spectators as stayed on to watch--and these were many. Night

came on steadily and Farman covered lap after lap just as steadily, a

buzzing, circling mechanism with something relentless in its isolated

persistency.

The final day of the meeting provided a further record in the quarter

million spectators who turned up to witness the close of the great week.

Bleriot, turning out in the morning, made a landing in some such fashion

as flooded the carburettor and caused it to catch fire. Bleriot himself

was badly burned, since the petrol tank burst and, in the end, only

the metal parts of the machine were left. Glenn Curtis tried to beat

Bleriot's time for a lap of the course, but failed. In the evening,

Farman and Latham went out and up in great circles, Farman cleaving his

way upward in what at the time counted for a huge machine, on circles

of about a mile diameter. His first round took him level with the top of

the stands, and, in his second, he circled the captive balloon anchored

in the middle of the grounds. After another circle, he came down on a

long glide, when Latham's lean Antoinette monoplane went up in circles

more graceful than those of Farman. 'Swiftly it rose and swept round

close to the balloon, veered round to the hangars, and out over to the

Rheims road. Back it came high over the stands, the people craning their

necks as the shrill cry of the engine drew nearer and nearer behind the

stands. Then of a sudden, the little form appeared away up in the deep

twilight blue vault of the sky, heading straight as an arrow for the

anchored balloon. Over it, and high, high above it went the Antoinette,

seemingly higher by many feet than the Farman machine. Then, wheeling

in a long sweep to the left, Latham steered his machine round past the

stands, where the people, their nerve-tension released on seeing the

machine descending from its perilous height of 500 feet, shouted their

frenzied acclamations to the hero of the meeting.

'For certainly "Le Tham," as the French call him, was the popular hero.

He always flew high, he always flew well, and his machine was a joy to

the eye, either afar off or at close quarters. The public feeling for

Bleriot is different. Bleriot, in the popular estimation, is the man who

fights against odds, who meets the adverse fates calmly and with good

courage, and to whom good luck comes once in a while as a reward for

much labour and anguish, bodily and mental. Latham is the darling of

the Gods, to whom Fate has only been unkind in the matter of the Channel

flight, and only then because the honour belonged to Bleriot.

'Next to these two, the public loved most Lefebvre, the joyous, the

gymnastic. Lefebvre was the comedian of the meeting. When things began

to flag, the gay little Lefebvre would trot out to his starting rail,

out at the back of the judge's enclosure opposite the stands, and after

a little twisting of propellers his Wright machine would bounce off the

end of its starting rail and proceed to do the most marvellous tricks

for the benefit of the crowd, wheeling to right and left, darting up and

down, now flying over a troop of the cavalry who kept the plain clear of

people and sending their horses into hysterics, anon making straight

for an unfortunate photographer who would throw himself and his precious

camera flat on the ground to escape annihilation as Lefebvre swept over

him 6 or 7 feet off the ground. Lefebvre was great fun, and when he had

once found that his machine was not fast enough to compete for speed

with the Bleriots, Antoinettes, and Curtiss, he kept to his metier of

amusing people. The promoters of the meeting owe Lefebvre a debt of

gratitude, for he provided just the necessary comic relief.'--(The Aero,

September 7th, 1909.)

It may be noted, in connection with the fact that Cockburn was the only

English competitor at the meeting, that the Rheims Meeting did more than

anything which had preceded it to waken British interest in aviation.

Previously, heavier-than-air flight in England had been regarded as

a freak business by the great majority, and the very few pioneers who

persevered toward winning England a share in the conquest of the air

came in for as much derision as acclamation. Rheims altered this; it

taught the world in general, and England in particular, that a serious

rival to the dirigible balloon had come to being, and it awakened the

thinking portion of the British public to the fact that the aeroplane

had a future.

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