CHAPTER VII

TYPES OF AËROPLANES

France has indeed been the breeding-place for types of aëroplanes.

From France have the nations of late been largely gathering them--save

Germany. She has preferred to evolve her own distinctive types.

Even before Wilbur Wright appeared with his machine at Le Mans and

the details were known, hearsay of his doings had fired the French

imagination to do what he had done. In ignorance of the vital principle

of movable surfaces that the Wrights had evolved, there came into

existence the unbending, rigid type that was not destined to survive.

The first of these was the bird of prey of M. Santos Dumont. Rudely

simple was it in its construction. Two box kites formed the supporting

surface. In the centre was the motor, with the screw behind. To attain

flight the machine was run upon wheels along the ground until a certain

speed was reached, when the machine rose into the air. With this the

inventor did not do much more than make aërial jumps; but rude as it

was it contained one feature which has since been retained in all

aëroplanes. In this one respect it was an advance--and a very necessary

one--upon the Wright machine. That feature was the attachment of

wheels to the machine that has been mentioned above. This was, indeed,

an important step in the evolution of the aërial scout. Had it been

necessary to continue using the external starting catapults that were a

feature of the early experiments of the Wrights, the application of the

aëroplane to warfare would have been somewhat limited.

The well-known Voisin machine was another outcome of this period, but,

imperfect as it was, it brought Mr. Henry Farman into fame, for on it

he was the first man in Europe to fly any distance worthy of mention.

THE FARMAN BIPLANE.

Discontented with the Voisin machine, Mr. Henry Farman constructed one

of his own design. Though it appeared at an early stage of aëroplane

development, it still remains one of the most efficient types of

biplanes. It has been used enormously in France, and armoured Farmans

play an important part in the great war that is proceeding.

Mr. Farman quickly realised that for maintaining lateral stability the

vertical planes fitted between the main planes of the Voisin type were

a very poor substitute for the wing-warping method of the brothers

Wright. He, however, produced the movement of the main surfaces in

an original manner. He hinged small flaps to the rear extremities of

the main planes. These he called “ailerons.” They produce much the

same effect as the wing-warping method of the brothers Wright. When

the biplane tilted sideways, the flaps were drawn down on the side

that was depressed. The pressure of the air on the flaps forced the

aëroplane back on an even keel. In the normal condition the flaps

flew out straight in the wind on a level with the main planes. Another

noticeable feature of Mr. Farman’s machine was the production of the

first light and efficient landing chassis. This was a combination of

wooden skids and bicycle wheels. Below the biplane, on wooden uprights,

he fitted two long wooden skids. On either side of each skid he placed

two little pneumatic tyred bicycle wheels, connected by a short axle.

These were held in position on the skid by stout rubber bands passing

over the axle.

In a general way the wheels raised the skids from the ground, but if

the ascent was abrupt the wheels were forced against the rubber bands

and the skids came in contact with the ground. With the abatement of

the force of the shock the wheels came again into play.

Simplification of the chassis is becoming evident in the latest forms

of all military aëroplanes, the reduction of weight in this portion of

the apparatus being important.

To Mr. Farman belongs the credit of having first applied to his

aëroplane the now famous Gnome motor, in which seven or more cylinders

revolve. It can truly be said that the influence of this motor on

facilitating flight generally, and very particularly military aviation,

has been nothing short of prodigious. The aëroplane, like the airship,

had to wait for the light petroleum motor. Its advent made flight

possible, but achievement in flight would have been comparatively small

had it not been for the welcome appearance of a motor specially adapted

to the purpose.

The early forms of aëroplane engines in which the cylinders were fixed

had proved to be quite unreliable owing to the high speeds at which

the engines had to work. Overheating, loss of power, and stopping

were frequent occurrences. The water-cooling and air-cooling systems

introduced were equally inefficient. The very fact that the cylinders

of the Gnome motor revolved effected the desideratum of automatic

cooling, and also gave a smooth, even thrust to the propeller.

If the aëroplanes in the present war were flying over the enemy’s lines

with old-fashioned engines, they would be dropping down into hostile

hands as quickly as dying flies from the ceiling on the first winter

days.

After the introduction of the Gnome motor, it was quickly realised that

the speeds secured by its use gave the aëroplane a stability that was

absent in the more slowly moving machines. Winds that were the bugbear

of the aëroplanists could then be combated, and the aëroplane ceased

to be the fine-weather machine. Heights could then be climbed that a

little while before were undreamt of. It is said that there are some

disadvantages in the case of revolving cylinders--that they have been

known to produce a gyroscopic effect that has upset the machine. This,

however, is a somewhat doubtful point. It may be urged that the greater

silence of motors with fixed cylinders is an advantage in war. This may

sometimes be so, and it is quite possible that for offensive aëroplanes

a special type of motor may be in the future evolved.

To return to the other features of the Farman machine. The plan he

adopted in his racing machines of making the upper plane larger than

the lower one was a valuable step in speed-producing machines.

The records won by Mr. Farman with his machines alone testify to

its efficiency. Often he has held the world’s records of distance,

duration, and height, wrestling, indeed, for these with the Blériot

monoplane.

In 1911 Mr. Farman began to make types of biplanes specially designed

for military use, and in which he studied how he could best give the

observing officer an unobstructed view of the ground beneath him. He

placed both pilot and observer in seats projecting in front of the main

planes. He also made a new departure in placing his upper plane in

advance of the lower one. He claimed that this facilitates climbing and

descent. He has, however, quite lately evolved a newer type of scouting

machine.

In this the lower plane is only one-third the span of the upper one.

The nacelle is not mounted on the lower plane, as in the ordinary

types of his machine, but, instead, strung from the main spars of the

top one. The usual chassis is absent. There is a single running wheel

mounted at each end of the lower plane, which is brought very close to

the ground. The upper and lower planes are separated by four pairs of

struts. The tail is similar to that used on the ordinary type.

The following are the dimensions of one of the latest 1914 types of

one-seated Farman machines:--

Length 3.75 metres

Span 11.50 metres

Area 26 sq. metres

Weight (total) 290 kgs.

„ (useful) 175 kgs.

Motor 80 h.p. Gnome

Speed 110 km. per hour

The following are the details of one of his high-power hydroplanes

(1914):--

Length 8.80 metres

Span 18.08 metres

Area 50 sq. metres

Weight (total) 605 kgs.

„ (useful) 275 kgs.

Maximum speed 105 km. per hour

[Illustration:

[_Topical Press._

A BLÉRIOT MONOPLANE IN FLIGHT,

showing one of the two wings attached to the tubular body of machine,

chassis, stabilising plane, and rudder at rear.]

THE BLÉRIOT MONOPLANE.

At the same time that Mr. Henry Farman was making his first flights on

his biplanes, M. Blériot was experimenting with monoplanes. His first

attempts were disastrous. Time after time he was dashed to the ground.

But he persevered, and produced a machine which by its performance

staggered the aëronautical world.

When he was first experimenting most people thought that it was

in superposed surfaces that success alone lay. They forgot the

researches of Langley. These had showed that support depended on

two factors--speed and surface; that when speed is increased a less

supporting surface will suffice. The success of Blériot took the world

by surprise. If I were asked to name the men who have done most to

further practical aëronautical development, I should unhesitatingly

say: 1, the brothers Wright; 2, Blériot; 3, Pégoud.

The first have been already dealt with. I will speak of the two latter

together.

Of the work of both there has been one underlying

characteristic--simplicity. The former has produced a machine stripped

indeed of encumbering complexities, in which the restriction of

accessories to what is absolutely necessary is carried to a fine art;

the latter with that very machine has performed experiments in the air

that the most sanguine enthusiast of a few years back would have deemed

far beyond the region of the possible. In his graceful air diving,

looping the loop, and flying upside down, he gave the world a great

object-lesson of the materiality of air. He showed the air can give the

aviator as much support as the water can to a fancy swimmer. He showed

that if the aëroplane is an unstable thing, the human brain can supply

the stability; that in human flight, like the bird and its wings, the

machine and individual can be in closest touch. No one has stripped

the air of its terrors as has M. Pégoud. In the yielding air there is

indeed safety! It is the ground the aviator has to fear!

I have spoken of the simplicity of the Blériot monoplane. In the

machine with which M. Blériot flew over the Channel in 1909, stretched

like the wings of a bird on either side of a tubular wooden frame

partly covered with canvas and tapering to the rear, are placed the two

supporting planes, rounded at the ends. At the front end is placed the

motor (in the original type a three-cylindered engine, now replaced by

the Gnome motor), geared direct to a 6 feet 6 inches wooden propeller,

and on a level with the rear end of the planes. Immediately behind

the engine is the petrol tank, and behind that the aviator’s seat.

Near the rear end of the frame and underneath it is the fixed tail,

with two movable elevating tips. How simple is the working of this

monoplane! Moving a lever backwards and forwards actuates the tips of

the fixed tail at the back of the machine, and causes it to rise or

fall. Moving the same lever from side to side warps the rear surfaces

of the supporting planes. The act of pushing from side to side a bar on

which the aviator’s feet rest puts the rudder into action and steers

the machine.

The triumphs of the Blériot monoplane would fill many pages. It was

the first machine to fly over an expanse of water--the Channel. Later,

it carried M. Prior from London to Paris without a stop, traversing

250 miles in three hours 56 minutes, beating the performances of the

fleetest express trains by three hours. If it no longer for the moment

holds the record of height, which it has so often done, it carried M.

Garros up to a height of 5,000 metres. When his engine broke down at

that prodigious height, by its superb gliding powers it brought him

safely to earth!

It has flown over the Alpine peaks! It carried the first aëroplane

post--1,750 letters and cards--from Hendon to Windsor in seventeen

minutes!

In 1911 Blériot No. XI. flew with ten persons on board.

Its past records have indeed fitted it to be a military machine. It

is doubtlessly destined to play an important rôle in the present war

in the hands of the French aviators. Especially suitable is this type

for the one-seated military machine. Often it may be desirable to

employ a two-seated machine to carry pilot and observer; but there is

often, too, a use for the single-seated type of machine flying at a

rate of some eighty miles an hour. The work of these observers is to

make swift dashes over the enemy’s lines, make a speedy reconnaissance

of the enemy’s position, and return at once to headquarters with what

information has been obtained.

The following are the dimensions, etc., of the 1914 type of armoured

Blériot monoplanes:--

Length 6.15 metres

Span 10.10 metres

Area 19 sq. metres

Motor 80 h.p. Gnome

Speed 100 km. per hour

THE ANTOINETTE MONOPLANE.

There is another monoplane that will figure in the history of

aëronautics--the Antoinette monoplane. This was the first flying

machine to fly in a wind. Up to the time that Mr. Latham went to the

flying meeting at Blackpool, which took place almost immediately after

the famous Rheims meeting, aviators had only dared to fly in calm

weather. On the flying grounds there used to be tiny flags on posts.

When the flags hung down limply that was the time for flying. When they

moved about, even languidly, that was the time to put the aëroplane

to rest in its shed. Aviators then underestimated the capabilities of

their own machines.

When the aviators came to England the island breezes kept the little

flags vigorously moving about. The aviators were consternated. The

public was disappointed. It began to regard flight as a calm-weather

business. Aëroplanes could not face one breath of wind! Of what

practical use would they ever be!

Latham at that time had his Antoinette monoplane at Blackpool. It

consisted of large and strongly built wings, giving a surface of

about 575 square feet, set at a dihedral angle. The motor was some

60 h.p. At the back of the body of the machine were fixed horizontal

and vertical fins. There were hinged horizontal planes at the end of

the tail for elevating or lowering the machine. “Ailerons” were used

on the main surface for controlling lateral stability. One day, at

Blackpool, Latham went up in a very high wind, and remained in the

air for a considerable time. How much of the stability of his machine

was due to his dexterity, or how much to the machine, it is difficult

to say. Probably the fact that the wings were set at a dihedral angle

had much to do with it. He also had a much larger horse power than his

contemporaries, which no doubt contributed to his success. Anyhow, by

the Antoinette monoplane flight was redeemed from the reproach that

it was merely a pastime for ideal weather conditions. From that time

aviators have sought the winds as well as the calms. Now aircraft can

fly in winds of forty-eight or even fifty miles an hour! This step

of Latham gave a great impetus towards the military adoption of the

aëroplane. The military and naval mind tends to despise what is only

of use in the most favourable conditions. It had put aside the airship

till it could combat moderate winds. It did the same with the aëroplane.

The Wright, Farman, and Blériot machines may be described as the

parent types from which have sprung the large variety which at the

present time are at the disposal of the aviator. Amongst the various

types which have sprung from the parent forms we search in vain for

any underlying new principles, if we except the Dunne machine. There

is, however, in the various types plenty of variety of constructional

detail. Perhaps the two most important features of modern aëroplane

work are (1), the gradual substitution of steel in place of wood, and

the general strengthening of aëroplane construction; (2), the armouring

of vital parts of aëroplanes for the exigencies of warfare. Of this

latter innovation mention will be made later. Regarding the various

types of machines now available, it must suffice in this chapter to

especially mention a few which have features of special interest for

the purpose of warlike operations.

The success of the operations of the British aëroplanists in the war

is evidence of the efficiency of the apparatus being used. The British

military aëronautical authorities have evolved a very useful form of

aëroplane. In present circumstances, however, detailed description of

this must be omitted.

WEIGHT-LIFTING MACHINES.

i. _The Cody Biplane._--The Cody type was quite an experimental

machine. It should not, however, be without notice, as it was an early

effort towards the production of weight-lifting machines. These, in

the future, will have to be evolved if the aëroplane is to take a

large part in offensive operations. Scouting and offensive work call

for different types of machines. The Cody biplane had the largest

supporting surface that has been made, excepting that of Sir Hiram

Maxim’s flying machine. The two main surfaces were 52 feet in length,

7 feet 6 inches wide. They had a supporting surface of 775 square

feet. But this was small compared with the Maxim giant, which spread

4,000 square feet of surface. In the Cody machine the front elevators,

which bore some of the load, alone represented 150 square feet. The

two vertical rudders were at equal distances fore and aft of the main

supporting surfaces. A distinctive feature was the elevator. This was

in two separate parts, each of which could be moved independently

of the other. Cody adopted the method of the brothers Wright for

attaining lateral stability and steering--warping the main surfaces.

There were vertical and horizontal rudders operated by a single

steering wheel. Cody used generally an 80 h.p. engine, but in some of

his experiments he went up to 130 h.p. A peculiarity of the screws was

their greater width at the base than at the tips. The weight of the

machine was about one ton. Though it was such a large machine some

attempts were made to give it portability. The two ends of the main

decks, each 16 feet long, were removable. The girder supporting the

elevator could also be detached, as the rear rudder frame was made to

fold back against the body. With this machine Cody flew at excellent

speeds, averaging fifty miles an hour. On one occasion he was credited

with seventy miles an hour.

It was the Cody machine which won the first prizes which were open to

the world at the military trials in 1912. Of all the earlier practical

fliers in this country no one perhaps did so much to popularise flight

as Cody. His pluck and perseverance, despite the constant disasters

that were his lot, gained British appreciation, and all recognised that

if he was not a man of letters he was one of intuition. His well-known

man-lifting kite, unequalled indeed for the purpose for which it was

designed, was an example of the illuminating flashes that were wont to

cross his brain. It was not the product of calculation, but the happy

thought.

ii. _Maurice Farman Biplane._--A type of weight-carrying machine that

has survived is that designed by Mr. Henry Farman’s brother, Mr.

Maurice Farman. This machine has extensions to its main surfaces,

which enable it to carry a considerable weight. It has been found

capable of remaining in the air a very long time, which is an important

consideration for war use, especially when the aëroplane is on the

offensive. It is capable of flying at a very low speed. A disadvantage

is that it requires very skilful piloting, especially when used in high

winds.

THE BREGUET BIPLANE.

Very conspicuous in the Paris Salon exhibitions has been the Breguet

biplane. This is one of very advanced type; it is a military machine

_par excellence_. Simplicity and portability throughout are its

distinguishing features, and these are the essence of a machine

designed for war. One might almost call it a combination of monoplane

and biplane construction. There is the familiar tapering of the

framework, with controlling planes at the end, such as in the Blériot,

but two superposed planes, instead of the bird-like projecting wings

of the Blériot, are above and below the body of the machine. Steel

enters largely into the design. There is a maximum of supporting struts

between the main surfaces. These are constructed with thin metal

ribs, and are therefore flexible, an exceedingly important feature,

rendering the machine exceptionally stable in high and gusty winds.

For portability the main surfaces can be taken out of position in a

few minutes. By the excellent method of hinging the planes to the body

of the machine the former may be turned back and folded up beside the

body of the machine. The aëroplane can therefore be described as a

folding-up one. It can therefore travel on the road like a motor-car,

instead of having to be packed up and conveyed in a wagon. This method

of road conveyance would be impracticable with a machine with its wings

outspread.

THE SHORT DOUBLE-ENGINED AËROPLANE.

How many times have engines failed during flight on both monoplanes

and biplanes! How many tragedies have thus been enacted! Time and

experience indeed have mitigated this type of aërial disaster. The

improvement in engines has been one cause of salvation in this respect,

the practice of vol-planing the other. But even now from the seat of

war comes the news of engines that fail and machines that drop into the

realm of the enemy. The old proverb of having two strings to one’s bow

should apply to aëronautics.

The desideratum, indeed, is the duplication of such a vital part as

the motor. Considerations of weight have been the hindrance to engine

duplication. Mr. Short has given very special attention to this

matter, and has designed what appears to be an excellent machine,

undoubtedly of military value. The biplane is supplied with two Gnome

motors. One drives the screws in the front of the machine, and placed

a considerable distance apart. The other drives a single screw behind

the planes. In the ordinary way both engines run at moderate speed, but

if one fails the acceleration of the speed of the other will keep the

machine flying.

THE VENDÔME MONOPLANE.

A monoplane which has repute in France for strength, general aptitude,

and convenience is the Vendôme type. It has been especially commended

by experts on account of the quickness with which it can be put

together and dismantled. The only criticism to which it has been

exposed is, perhaps, that it is a little too strong for requisite

lightness, and that a modification of the metallic portions might

reduce weight without sacrifice of efficiency. This machine throughout

is made of hickory wood.

BREGUET-BRISTOL BIPLANE.

This is one of the newest machines France has at her disposal. It is a

happy combination of British and French make, due to the collaboration

of two firms, the Bristol Company and La Société Breguet.

The result of the combination is said to be eminently satisfactory. A

distinguishing feature of this machine is rapid dismantlement. There

are two pairs of wings. These are identical, interchangeable, and

connected in each case by a flexible partition, which permits of the

wings being laterally straightened up. The area of this interesting

machine is 39 square metres; length, 8.90 metres; span, 11.50 metres.

THE DESTROYER NIEUPORT MONOPLANE.

During this year, even before the outbreak of war, the aëroplane

had been well armoured and armed. A striking example of an armoured

air-scouting machine is the Nieuport monoplane. This type has obtained

brilliant result. Equipped with pilot, bombs, and armament it has

flown at the rate of 145 kilometres an hour, risen at the rate of 500

metres in 3 minutes 45 seconds, made its departure and landed within an

enclosure of 150 square metres.

This monoplane has 24 square metres of surface, and weighs more than

1,000 kgs. The armoury is carried out by a cuirass of steel or nickel

plates, which cover the vital front parts and the place where the pilot

sits.

ARMOURED CLEMENT-BAYARD MONOPLANE.

This new type is exceedingly well armoured, the protective caps

covering the motor and the middle of the machine.

The following are the dimensions, etc.:--

Length 5.60 metres

Span 9.50 metres

Area 18 sq. metres

Motor 100 h.p. Gnome

Weight 415 kgs.

Speed 150 km. per hour

On June 6th last the French military aviators with their armoured and

armed aëroplanes were reviewed at Villacoublay by General Joffre and

General Bernard, the director of military aëronautics. Amongst the

types of aëroplanes present was the Dorand biplane, having two Gnome

motors driving separate screws, armoured in its vital parts, and

armed with a Hotchkiss mitrailleuse. This was mounted on a pivot,

and could be fired in almost every direction. There were, too, the

Morane-Saulnier, Blériot-Gouin, Nieuport, and Breguet-Bristol types.

M. Raymond, in his speech before the Senate in February last, said

that Germany was in possession of armoured aëroplanes, but that France

had none. The June review at Villacoublay showed what vast strides in

military aëroplane construction the French had made in a few months.

The French military aëroplanes consist of Farman types, and many other

leading French forms. In 1913 there were about 500 French military

aëroplanes and a few naval hydroplanes.

France manufactures a great number of aëroplanes, of late years about

1,000 per year. These include Government machines, those of private

owners and export machines. There are at least twenty-nine French

flying grounds, many of them flying schools and trial grounds of the

leading French airship and aëroplane makers.

In 1913 Italy appears to have had about a hundred military aëroplanes,

including those on order, Blériots, Bristol (monoplanes), Farmans,

Nieuports, and others. She had six or eight naval aëroplanes. She is

well provided with military flying schools and other flying grounds,

nearly all fitted with hangars.

There are military airship hangars at Rome, Milan, Verona, Venice, and

Bracciano.

Belgium has a military school of aviation near Antwerp, and in 1913

she had as many as twenty-four military aëroplanes--H. Farman, 80 h.p.

Gnome. There are in Belgium about half a dozen flying grounds, and as

many aërial societies or clubs.

As already stated, Germany, in the first instance, looked to

Austria-Hungary for her aëroplanes, and the Etrich was an Austrian

machine. In late years, however, Austria’s aëroplanes were mainly

Lohners; the Government favoured this make and discouraged others,

consequently enterprise and invention languished. After the accident to

the Aspern the Lohner was condemned as of too feeble a resistance, and

meanwhile discouragement had effaced all the other systems.

Aëroplanes are used both in the Russian army and navy. Those of the

navy are hydro-aëroplanes, or capable of being so arranged. In number,

the Russian navy has about a dozen. Of military aëroplanes Russia has

probably from 250 to about 300, many of them of modern type, and built

in Russia, the principal types being Rumpler, Albatross, Aviatik,

Nieuport, Farman, Bristol and Deperdussin.

Bulgaria has a number of aëroplanes, mainly Blériots and Bristols.

SYKORSKY’S GIANT AËROPLANE.

A very remarkable type of aëroplane is the giant biplane invented by

the Russian aviator Sykorsky. It doubtless marks the beginning of

a new era in the construction of machines on the heavier-than-air

principle. Most aviators have shirked the use of a machine that could

carry a large number of persons. It would seem that Russia is destined

to take the lead in this class of machine, which may before long put

the lighter-than-air Zeppelins entirely out of date. The machine

of Sykorsky is not, indeed, a mere project, but a reality, for at

Petrograd on February 25th, it flew for eighteen minutes with sixteen

passengers on board. They represented a weight of 1,300 kilogrammes.

The height attained in this flight was 300 metres. On February 27th the

machine flew from Petrograd to Tsarskoe Selo and back again, taking

nine persons, in two hours six minutes, at a height of 1,000 metres.

The performance constituted a triple record of distance, height, and

duration of flight with nine persons on board.

The following are the dimensions, etc.:--

Length 20 metres

Span 37 metres

Surface 182 sq. metres

Distance between planes 2.80 metres

Motive power 4 Argus motors (100 h.p. each)

Weight of motors 220 kgs.

Weight of machine without

passengers 3,500 kgs.

Weight with 16 passengers 4,800 kgs.

The motors are placed in groups of two on each side of the body of the

machine. Each pair works a screw and each individual motor can be put

into action and stopped separately. The body of the machine contains a

chamber for the pilots three square metres in size, a passenger salon

of five square metres, and two other chambers of three and two square

metres respectively. The whole are lit by four windows on each side.

The rooms can be artificially lighted by electricity and warmed by

motor gas. There are, indeed, future possibilities for such a machine

in war!

I have mentioned that the type of aëroplane devised by Lieutenant Dunne

is characterised by a distinctive principle of its own. The claim is

made that it is automatically stable. It has, however, rather a claim

to “inherent stability” than “automatic stability,” if we accept the

terms as Professor Bryan has defined them.

The following details appeared in the “Aëronautical Journal”:--

The salient features of the machine are the backward slope of the

planes, which, in plan view, form an angle with the apex in the

direction of flight, and the absence of a tail or supplementary

planes of any description. The following are its chief

dimensions:--Span, 46 feet; length (fore and aft), from apex to

rear wing tip, 20 feet 4½ inches; length of body, 19 feet; surface,

500 square feet; weight (including pilot and six gallons of

petrol), 1,700 lb.; engine, four-cylinder 50–60 h.p. Green, 1,100

r.p.m., driving twin propellers placed one on either side of the

body in the rear.

The weight in flight being 1,700 lb., the aëroplane carries a load

of about 3 lb. per square foot. The speed in flight averages about

40 m.p.h.

The chord of the surfaces is even throughout--6 feet; the vertical

distance between the surfaces is also constant at 6 feet; at

either extremity a vertical curtain is placed between the surfaces

to prevent leakage of air sideways. The surfaces slope back from

the apex at an angle of 58° on either side, the rear wing tips,

therefore, actually being in the rear of the aft end of the body,

and the entire outer extremities of the wings lying back well

behind the centre of gravity.

The curve or camber of the planes is not uniform, and, briefly,

it may be said that each wing may be viewed as a portion of the

surface of a cone with the apex to the rear. A consequence of this

is that the angle of incidence of each wing gradually decreases

from the root to the tip; so much so, that while the angle at

the root is positive, that at the tip is distinctly negative,

the difference in the respective angles being 45°. Apart from

this, an interesting feature is the extreme downward bend of the

_trailing_ edges over a short distance where the two surfaces

meet in the centre; this arrangement has been adopted chiefly

to enable the aëroplane to right itself naturally in the event

of its having assumed a vertical position in the air. A further

interesting consideration is that this machine is the only one

that could safely be forced backwards. It may be added, briefly,

that the loss in efficiency arising from the negative angle of the

wing-tips is compensated by the backward slope and angle of the

surfaces, which naturally causes the flow of air to be depleted

outwardly beneath the planes, and even induces a certain amount of

compression beneath the outer ends. The body is entirely covered

in; the pilot’s seat is in the prow; the motor further to the rear.

The centre of gravity is well forward, and about six inches above

the lower plane. The propellers are carried on a transverse girder,

and are chain-driven in the same direction--contra-clockwise

viewed from the rear. The centre of the boss is situated 1 foot

2 inches above the lower plane, and 4 feet from the central axis

of the machine. The propellers, designed by Capt. Carden, are

of solid wood, 7 feet in diameter, 7 feet 6 inches pitch, each

weighing 21 lb. The chassis comprises two main wheels, with a small

wheel-and-skid fore and aft. The system of controls is extremely

simple. The trailing edge of each extremity of the upper plane

forms a hinged flap, measuring 7 feet 2 inches by 1 foot 9 inches.

These are independently controlled by two levers, one on either

hand of the pilot a couple of mirrors allow the pilot to ascertain

the working of the steering-flaps when in flight. The throttle

control is fixed to the right-hand lever.

On several occasions, while flying on this machine, the pilot used both

hands for writing and making notes, leaving the machine uncontrolled,

and came down with his hands raised above his head.

Germany has many forms of aëroplanes, and these will be treated of in

the next chapter.

[Illustration: _AVIONS ALLEMANDS_

TIREZ

sur ces Appareils

MONOPLAN TAUBE

TAUBE

MONOPLAN GOTHA

GOTHA

MONOPLAN RUMPLER

RUMPLER

BIPLAN ALBATROS

ALBATROS

ZEPPELIN

A DIAGRAM ISSUED BY THE FRENCH WAR OFFICE FOR THE GUIDANCE OF THE MEN

IN THE TRENCHES.

It gives a silhouette of some Aëroplanes and an Airship in the German

service, and bears the injunction--“German Aëroplanes--fire on these

machines.”]

Aircraft in war · 第 7 / 11 章