Their control of the machine was even better than they had dared to

expect. They got quick response to the slightest movement of the front

elevator, which promised to be satisfactory in maintaining fore and

aft balance. At first, they fastened the warping mechanism, to make it

inoperable, and had only the elevator to manipulate, for they feared

that, inexperienced as they were, if they tried to use both, then

they might be unsuccessful with either. But even without the use of

the warping mechanism it was possible to make glides of from five to

ten seconds before the sidewise tilt of the machine forced a landing.

Before making the last three or four flights the Wrights loosened the

warping wires to permit the sidewise control to be used.

When these experiments of 1900 ended, instead of the hours of practice

in the air the Wrights had hoped to have, they had flown the machine

as a kite with a man aboard barely ten minutes, and had had only two

minutes of actual gliding.

Now that the experiments for that year were ended and they had no

further use for the glider, the brothers weighted the machine with sand

and left it on the hill. When “Bill” Tate saw that they were through

with the glider he asked if he might have it, and they gladly gave

it to him. Mrs. Tate used the sateen that covered the wings to make

dresses for her two small daughters. She noted that it appeared to

be unusually good fabric, more closely woven and better than she had

seen in the stores. Some of her neighbors, when they saw the dresses

she made of it, remarked that it seemed too bad to use such excellent

material on a kite.

Though the amount of practice was less than they had expected, all

the Wrights had learned in that season of 1900 seemed to confirm the

correctness of certain opinions held at the beginning. Their method of

warping or twisting the wings to maintain lateral balance was better

than dependence on either the dihedral angle or shifting the weight

of the operator; better than any method yet tried. And their front

elevator had been highly satisfactory as a means for directing the

machine up and down. Before leaving Kitty Hawk they decided that their

next experiments would be with a glider large enough to be flown as a

kite, with an operator aboard, in winds ordinarily to be counted on.

When the brothers set to work on their glider for the experiments of

1901, they decided to make it of the same general design as the first

one, and with the same system of control. But they carried out their

plan to give it considerably more area, to provide greater lifting

power. Another change they made was to increase the curvature of the

wings to conform to the shape on which Lilienthal had based his tables

of air pressures. It had wings of about seven-foot chord (the straight

line distance between the front and rear edges) with a total span of

twenty-two feet, and weighed ninety-eight pounds. After a section

twenty inches wide had been removed from the middle of the lower wing,

and the rear corners of the wings rounded off, the total lifting area

was 290 square feet, as compared with 165 in the previous glider. The

front elevator, with its rear edge about two and one half feet away

from the front edge of the wings, had a four-and-one-half foot chord

and an area of eighteen square feet.

This was a much larger machine than anyone had ever tried to fly. The

Wrights knew it could not be controlled simply by shifting the pilot’s

weight, as others had done, but they had faith in their own operable

front elevator and believed they could manage it. If their calculations

were correct, it would be supported in a wind of seventeen miles an

hour, with the wing surfaces at an “angle of incidence” of only three

degrees. (“Angle of incidence,” now more often called “angle of

attack,” has been defined as the angle at which the plane presents

itself to the air in advancing against it.)

As it would be impractical to keep so large a machine with them in the

tent, as they had done with the smaller glider, the brothers built near

Kill Devil Hill a rough frame shed, twenty-five feet long, sixteen

feet wide, and seven feet high at the eaves. Both ends of the building

except the gable parts were made into doors, hinged above. When open,

the doors provided an awning at each end of the building. For living

quarters they still used a tent. By driving a pipe ten or twelve feet

into the sand they got a water supply.

Though the great stretch of sandy waste seemed too desolate for

anyone to bother about owning, yet it was all under the ownership of

one person or another and the Wrights took the precaution to obtain

permission to erect their buildings.

This year they were to have company in camp. Octave Chanute, with whom

they had been in correspondence for about a year, stopped in Dayton

in June, 1901, at their invitation, to get better acquainted. When

he learned that the Wrights had carried on their experiments in 1900

without the presence of a doctor in camp, and were intending to do so

again, he told them he thought that was too risky, considering the kind

of work and the isolation of the experiment ground. He said he knew a

young man in Coatesville, Pennsylvania, George A. Spratt, “an amateur”

in aeronautics, who had had some medical training. Spratt had never

seen any gliding experiments, and Chanute thought he would be eager

for the opportunity. If the Wrights would board him at camp, Chanute

said, he would be glad to pay Spratt’s traveling expenses to Kitty Hawk

and would consider himself “compensated by the pleasure given to him.”

Chanute also proposed that they have in camp with them E. C. Huffaker,

of Chuckey City, Tennessee, who was building a glider that Chanute was

financing, and the Wrights consented. Thus there were four regularly

in camp that season, and for a time Chanute himself was with them as a

guest.

The new machine was completed and ready for trial on the afternoon

of July 27. Since it was designed to be flown in a wind of seventeen

miles, and there was but thirteen miles of wind on that day, the

brothers took the machine to the big Kill Devil Hill for its first

trial. After five or six short tuning-up flights they made a glide of

315 feet in nineteen seconds. Although several flights on this first

day of experiments in 1901 exceeded the best made the year before,

yet it was soon evident that in several respects the machine was not

as good as the first one. It was found that the wings, with a camber

of one to twelve--the camber recommended by Lilienthal, and used by

Chanute and others--was not so good as the camber of one to twenty-two,

used by the Wrights in 1900. (Camber of one to twenty-two means that

the length of the chord, the straight-line distance between the front

and rear edges of the wings, is twenty-two times the distance _from_

the chord to the deepest part of the wing curve.) This was demonstrated

by the fact that the 1901 machine could not glide on a slope as nearly

level as had the earlier machine. The Wrights found, too, that a

machine with wings of one to twelve camber was not so easily controlled

fore and aft as when the wings were of one to twenty-two camber. They

decided therefore to reduce the camber of the wings to make them more

like those of the earlier machine. When they resumed their gliding,

after the camber had been reduced (one to eighteen), the control of

the machine appeared to be as good as it was the year before, and they

then made flights in winds of twenty-two to twenty-seven miles an hour,

without accident. Though in most of these flights the lateral control

was highly effective, in a few others--under conditions seemingly the

same--the wing warping appeared to have no effect at all.

The Wrights now made the discovery that in free flight, when the wing

on one side of the machine was presented to the wind at a greater

angle than that on the other side, the wing with the greater angle,

instead of rising as it was expected to do, sometimes descended. The

explanation was that the greater angle of the wing at one side gave

more resistance to forward motion and thus reduced the speed on that

side. This decrease in speed more than counter-balanced the effect of

the larger angle of the wing in producing lift. (The Wrights had not

discovered this when flying the glider as a kite, because, when held by

ropes, the wings always maintained equal air speeds, even when their

resistances were unbalanced.)

It was evident to the brothers that their present method of controlling

equilibrium was not yet complete. Something was needed to maintain

equal speeds at the two wing tips. The idea occurred to them that the

addition of a vertical fin attached to the machine at some distance in

the rear of the wings might be the solution of the problem. But the

test of such a fin had to be left until another season.

The behavior of the glider in these various flights forced the Wrights

to give thought to another scientific problem, that regarding the

center of air pressure on curved surfaces. Contrary to the teachings of

scientific books on the subject, it was becoming more and more evident

that the travel of the center of pressure on a cambered surface is not

always in the same direction as the travel on a plane surface. When

the angle of attack on a plane surface is decreased, the center of

pressure moves toward the front edge; but on a cambered surface this

is true only when larger angles are being decreased. When the angle of

attack on a cambered surface is decreased from, say, thirty degrees

to twenty-five degrees, the center of pressure moves forward, as it

does on a plane surface; but when a certain angle (between twelve

and fifteen degrees) is reached, then the movement of the center of

pressure is reversed. From there on, the center of pressure moves

toward the rear so long as any further decrease is made in the angle

of attack. The Wrights proved this by a series of experiments with a

single surface from their plane. Knowledge of the phenomenon of this

reversal of center of pressure was of great importance to them in their

later work of designing aeroplanes.

Scientific problems were not the only ones to perplex the Wrights. A

sore trial were the mosquitoes and sandfleas, particularly numerous

and aggressive in that summer of 1901. As Orville Wright recalled

in later years, there were times when he thought, while fighting

mosquitoes through the night, that if he could just survive until

morning he would pack up and return home. Those mosquitoes might have

caused a long postponement of the conquest of the air.

By the time they left Kitty Hawk on August 20, the brothers had

satisfied themselves that a glider of large surfaces could be

controlled almost as easily as a smaller one, provided the control is

by manipulation of the surfaces themselves instead of by movements

of the operator’s body. So far as they knew, judging from figures

previously published, they had broken all records for distance in

gliding. Chanute, who had witnessed part of the 1901 experiments,

insisted that the results were better than had ever been attained

before. All that was encouraging. But, on the other hand, if most of

the supposedly scientific information available was worthless, then

their task was even more formidable than they had expected. With no

dependable previous knowledge to guide them, who were they to determine

how man should fly? Wilbur seemed much discouraged. Possibly he had

entertained hopes of actually flying, though he had always disclaimed

having such an idea. He was ready to drop the experiments altogether.

On the way home, Wilbur declared his belief: Not within a thousand

years would man ever fly!

Chanute urged the brothers not to drop their experiments, arguing that

if they did it would be a long time before anyone else would come as

near to understanding the problem or how to work toward its solution.

Without knowing it, Chanute made a great contribution to aviation

history, for the Wrights heeded his repeated admonitions against

ceasing their efforts. Without the proddings of Chanute they might not

have gone on.

Chanute performed another great service for aeronautics when he, as

president of the Western Society of Engineers, invited Wilbur Wright to

address that body at a meeting in Chicago, September 18, 1901, on the

subject: Some Aeronautical Experiments.

Wilbur shrank from the idea of making such a talk and would hardly have

done so except to oblige his friend. He cautioned Chanute, though,

not to make the speech a prominent feature of the program, because,

he said, he made no pretense of being a public speaker. Chanute did

nevertheless plan to use the announcement of the talk as a means to

help make the meeting a big success. He wanted to know if it would be

all right to make the occasion “Ladies’ Night.” Wilbur decided that he

would already be as badly scared as a man could be and the presence of

women would not make the situation much worse. But he insisted on one

thing, that he must not be expected to appear in formal evening dress.

In this speech Wilbur boldly declared that the best sets of figures

obtainable regarding air pressure against airplane surfaces appeared

to contain many serious errors. Orville, at the shop in Dayton, was a

little alarmed about that part of the speech. What if something about

their own work had been wrong and the figures compiled by various

scientists should finally be proved correct? Certainly it was no small

responsibility for anyone so little known as Wilbur or he to denounce

publicly the work of eminent scientists, dignified by preservation in

books long regarded as authoritative. It would be both presumptuous and

risky to brand supposedly established facts as untrue unless the person

doing so could be unassailably sure of his ground.

In this cautious state of mind Orville rigged up a little wind-tunnel

for the purpose of making a series of tests. This tunnel consisted

simply of what appeared to be an old starch box, not more than eighteen

inches long, that was lying in the shop. In it he placed a hastily

constructed apparatus, a main part of which was simply a metal rod

pivoted in the manner of a weather vane. Without attempting to give

technical details of the method used, it may be said that a curved

surface was balanced against a plane surface in an air current passing

through the box. As Orville had provided the box with a glass top he

could measure the angles to the wind at which the curved surface and

the plane surface of equal area produced equal pressures.

The experiments with this crude apparatus lasted only one day. They

were conclusive enough so far as they went, indicating errors in

published figures relating to air pressure on curved surfaces. But

as Orville was later to learn, the published errors were greatest in

regard to wing surfaces set at small angles, such as would be used in

flying, and he had tested thus far only larger angles. With the tests

thus incomplete, Orville and Wilbur decided, on the latter’s return

from Chicago, that it might be prudent to stay on the safe side and

omit from the published record of Wilbur’s speech the more severe

part of his criticism of available figures. They would wait until

further wind-tunnel experiments could give more detailed knowledge.

Consequently, when Wilbur’s speech appeared in the December, 1901,

issue of the _Journal of the Western Society of Engineers_, it was a

bit less startling than the one he had actually delivered--though, even

after the deletions, there still remained strong hints that accepted

tables of figures might be wrong. And the record of the speech was

treated as of great importance. It has probably been reprinted and

quoted as often as any other article ever written on the subject of

flying.

The Wrights were not sure they would ever build another glider. But

their curiosity, their passion for getting at truth, had now been too

much aroused for them to quit studying the problem of air pressures.

They decided to build another wind-tunnel, less crude than the one

Orville had hastily used, and continue their experiments. The new

tunnel consisted of an open-ended wooden box about sixteen inches

square on the inside by six feet long. Into one end would come a

current of air and the draft thus created would be “straightened,”

as well as made uniform, by having to pass through a set of small

pigeon-holes. It would have been a great convenience to use an electric

fan for sending the air into the tunnel. But the Wrights had no

electric current in their shop--still lighted by gas--and the fan was

driven by a one-cylinder gas engine they had previously made. They

attached the fan to a spindle that had held an emery wheel. A new

measuring device, or balance, was built of wire intended for bicycle

spokes, and pieces of hacksaw blades. These experiments were now done

with much more refinement than at first, and the measurements were

for both “lift” and “drift.” But as each curved surface measured was

balanced against the pressure on a square plane, exposed at ninety

degrees to the same air current, it was not necessary to know the

precise speed of the air current.

During that autumn and early winter of 1901, the brothers tested in

the wind-tunnel more than two hundred types of wing surfaces. They

set these at different angles, starting with the angle at which the

surface begins to lift, and then at 2½ degree intervals, up to twenty;

and at five degree intervals up to forty-five degrees. They measured

monoplane, biplane, and triplane models; also models in which one

wing followed the other, as used by Langley in his experiments. They

measured the lift produced by different “aspect ratios”--that is, the

ratio of the span of the wing to its chord. They found that the greater

the span in proportion to the chord the more easily the wing may be

supported. They measured thick and thin surfaces. One surface had a

thickness of nearly one-sixth of its chord.

Among other things, these experiments proved the fallacy of the sharp

edge at the front of an airplane wing and the inefficiency of deeply

cambered wings as then generally advocated by others. Sometimes they

got a result so unexpected that they could hardly believe their own

measurements--as, for example, when they discovered that, contrary to

all previously published figures by students of the subject, a square

plane gave a greater pressure when set at thirty degrees than at

forty-five degrees.

These wind-tunnel experiments in the bicycle shop were carried on for

only a little more than two months, and were ended before Christmas,

1901. The Wrights discontinued them with great reluctance; but, after

all, they were still in the bicycle business, still obliged to give

thought to their means for earning a living, and with no idea that

this scientific research could ever be financially profitable. In

those few weeks, however, they had accomplished something of almost

incalculable importance. They had not only made the first wind-tunnel

in which miniature wings were accurately tested, but were the first

men in all the world to compile tables of figures from which one might

design an airplane that could fly. Even today, in wind-tunnels used in

various aeronautical laboratories, equipped with the most elaborate

and delicate instruments modern science can provide, the refinements

obtained over the Wrights’ figures for the same shapes of surfaces

are surprisingly small. But it is doubtful if the difficulties and

full value of the Wrights’ scientific researches within their bicycle

shop are yet appreciated. The world knows they were the first to

build a machine capable of sustained flight and the first actually

to fly; but it is not fully aware of all the tedious, grueling

scientific laboratory work they had to do before flight was possible.

Important as was the system of control with which the Wrights’ name

has been connected, it would not have given them success without their

wind-tunnel work which enabled them to design a machine that would lift

itself.

The Wrights had a double reason for making sure of their figures.

With little money to spend on a hobby, it was much cheaper to rectify

mistakes on paper than after the idea was put into material form. They

knew that if they should decide to go on to further gliding attempts,

they could not afford to spend much more money on apparatus built

according to unreliable data.

After compiling their own tables of figures, the Wrights gave copies

of them to their friend Chanute and others interested in the problem

of aerodynamics. Chanute well knew that the Wrights now had knowledge

of aeronautics far beyond that of anyone else in the world, and he

felt that for them to go on with their experiments was almost a duty.

He much regretted, in the interest of science, he said, that they had

reached a stopping-place, for he was sure further experiments on their

part promised “important results.”

Chanute might well have felt pride in the effectiveness of his

insistence that the Wrights should go on experimenting, as well as in

the results of his invitation to Wilbur to make that Chicago speech.

Except for that speech and its daring statements that Orville thought

needed more confirmation, there probably would have been no wind-tunnel

tests; and without the kind of knowledge then obtained, neither the

Wrights nor anyone else could have built a practical flying-machine.

Those wind-tunnel experiments marked one of the great turning points in

the long history of attempts at human flight.

It still remained for the Wrights to put their new knowledge to actual

test in gliding, and they set out on August 25, 1902, for their third

stay at Kitty Hawk. But not until September 8 were they able to begin

the work of assembling their new glider, for the camp, battered by

winter gales, needed much repairing; and they decided to build an

addition to it for living quarters. They did not have their machine

ready for its first trial until September 19.

This new glider was of not much greater lifting area than that of

the previous year, though the wing span had been increased from

twenty-two to thirty-two feet. But since the wind-tunnel experiments

had demonstrated the importance of the “aspect ratio,” the total span

was now about six times the chord instead of three. One minor change

also may be noted. In the earlier gliders, the wing-warping mechanism

had been worked by movement of the operator’s feet; but now in this

1902 glider it was done by sidewise movement of one’s hips resting on

a “cradle.” The most noticeable change was the addition of a tail,

consisting of fixed twin vertical vanes, with a total area of a trifle

less than twelve square feet. Its purpose was to correct certain

difficulties encountered in some of the flights with the 1901 machine.

When the wing surfaces at the right and left sides were warped to

present different angles toward the wind, the wing that had the greater

angle, and therefore the more resistance, tended to lag behind, and

then the slower speed offset what otherwise would have been the greater

lifting power of that wing. The tail was expected to counter-balance

that difference in resistance of the wing tips. If the wing on one

side tended to swerve forward, on a vertical axis, then the tail, more

exposed to the wind on that same side, should, it was thought, stop

the machine from further turning.

Entirely apart from any advantages to be gained from the use of the

tail, the first trials of the new machine were highly encouraging for

another reason. It was soon evident that by disregarding all tables

of air pressures used by their predecessors and building according to

the figures obtained from their wind-tunnel experiments, the Wrights

had made a big advance toward flight. Because of the knowledge they

now had, not possessed by any previous experimenter, of how the wings

should be shaped, this 1902 machine was of just about twice the

“dynamic efficiency” of any other glider ever built; it could have been

flown with probably less than half the power required for any other

glider.

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