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´╗┐Title: The Early History of the Airplane
Author: Wright, Orville, 1871-1948, Wright, Wilbur, 1867-1912
Language: English
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Copyright Status: Not copyrighted in the United States. If you live elsewhere check the laws of your country before downloading this ebook. See comments about copyright issues at end of book.

*** Start of this Doctrine Publishing Corporation Digital Book "The Early History of the Airplane" ***

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The EARLY HISTORY of the AIRPLANE

  The DAYTON-WRIGHT AIRPLANE CO.
  DAYTON OHIO



The Wright Brothers' Aeroplane

_By Orville and Wilbur Wright_


Though the subject of aerial navigation is generally considered new, it
has occupied the minds of men more or less from the earliest ages. Our
personal interest in it dates from our childhood days. Late in the
autumn of 1878 our father came into the house one evening with some
object partly concealed in his hands, and before we could see what it
was, he tossed it into the air. Instead of falling to the floor, as we
expected, it flew across the room, till it struck the ceiling, where it
fluttered awhile, and finally sank to the floor. It was a little toy,
known to scientists as a "helicoptere," but which we, with sublime
disregard for science, at once dubbed a "bat." It was a light frame of
cork and bamboo, covered with paper, which formed two screws, driven in
opposite directions by rubber bands under torsion. A toy so delicate
lasted only a short time in the hands of small boys, but its memory was
abiding.

Several years later we began building these helicopteres for ourselves,
making each one larger than that preceding. But, to our astonishment, we
found that the larger the "bat" the less it flew. We did not know that a
machine having only twice the linear dimensions of another would require
eight times the power. We finally became discouraged, and returned to
kite-flying, a sport to which we had devoted so much attention that we
were regarded as experts. But as we became older we had to give up this
fascinating sport as unbecoming to boys of our ages.

It was not till the news of the sad death of Lilienthal reached America
in the summer of 1896 that we again gave more than passing attention to
the subject of flying. We then studied with great interest Chanute's
"Progress in Flying Machines," Langley's "Experiments in Aerodynamics,"
the "Aeronautical Annuals" of 1905, 1906, and 1907, and several
pamphlets published by the Smithsonian Institution, especially articles
by Lilienthal and extracts from Mouillard's "Empire of the Air." The
larger works gave us a good understanding of the nature of the flying
problem, and the difficulties in past attempts to solve it, while
Mouillard and Lilienthal, the great missionaries of the flying cause,
infected us with their own unquenchable enthusiasm, and transformed idle
curiosity into the active zeal of workers.

In the field of aviation there were two schools. The first,
represented by such men as Professor Langley and Sir Hiram Maxim,
gave chief attention to power flight; the second, represented by
Lilienthal, Mouillard, and Chanute, to soaring flight. Our sympathies
were with the latter school, partly from impatience at the wasteful
extravagance of mounting delicate and costly machinery on wings
which no one knew how to manage, and partly, no doubt, from the
extraordinary charm and enthusiasm with which the apostles of soaring
flight set forth the beauties of sailing through the air on fixed
wings, deriving the motive power from the wind itself.

The balancing of a flyer may seem, at first thought, to be a very simple
matter, yet almost every experimenter had found in this one point which
he could not satisfactorily master. Many different methods were tried.
Some experimenters placed the center of gravity far below the wings, in
the belief that the weight would naturally seek to remain at the lowest
point. It is true, that, like the pendulum, it tended to seek the lowest
point; but also, like the pendulum, it tended to oscillate in a manner
destructive of all stability. A more satisfactory system, especially for
lateral balance, was that of arranging the wings in the shape of a broad
V, to form a dihedral angle, with the center low and the wing-tips
elevated. In theory this was an automatic system, but in practice it had
two serious defects: first, it tended to keep the machine oscillating;
and second, its usefulness was restricted to calm air.

In a slightly modified form the same system was applied to the
fore-and-aft balance. The main aeroplane was set at a positive angle,
and a horizontal tail at a negative angle, while the center of gravity
was placed far forward. As in the case of lateral control, there was a
tendency to constant undulation, and the very forces which caused a
restoration of balance in calms caused a disturbance of the balance in
winds. Notwithstanding the known limitations of this principle, it had
been embodied in almost every prominent flying machine which had been
built.

After considering the practical effect of the dihedral principle, we
reached the conclusion that a flyer founded upon it might be of interest
from a scientific point of view, but could be of no value in a practical
way. We therefore resolved to try a fundamentally different principle.
We would arrange the machine so that it would not tend to right itself.
We would make it as inert as possible to the effects of change of
direction or speed, and thus reduce the effects of wind-gusts to a
minimum. We would do this in the fore-and-aft stability by giving the
aeroplanes a peculiar shape; and in the lateral balance by arching the
surfaces from tip to tip, just the reverse of what our predecessors had
done. Then by some suitable contrivance, actuated by the operator,
forces should be brought into play to regulate the balance.

Lilienthal and Chanute had guided and balanced their machines, by
shifting the weight of the operator's body. But this method seemed
to us incapable of expansion to meet large conditions, because the
weight to be moved and the distance of possible motion were limited,
while the disturbing forces steadily increased, both with wing area
and with wind velocity. In order to meet the needs of large machines,
we wished to employ some system whereby the operator could vary at
will the inclination of different parts of the wings, and thus obtain
from the wind forces to restore the balance which the wind itself had
disturbed. This could easily be done by using wings capable of being
warped, and by supplementary adjustable surfaces in the shape of
rudders. As the forces obtainable for control would necessarily
increase in the same ratio as the disturbing forces, the method
seemed capable of expansion to an almost unlimited extent. A
happy device was discovered whereby the apparently rigid system
of superposed surfaces, invented by Wenham, and improved by
Stringfellow and Chanute, could be warped in a most unexpected
way, so that the aeroplanes could be presented on the right and
left sides at different angles to the wind. This, with an adjustable,
horizontal front rudder, formed the main feature of our first glider.

The period from 1885 to 1900 was one of unexampled activity in
aeronautics, and for a time there was high hope that the age of flying
was at hand. But Maxim, after spending $100,000, abandoned the work;
the Ader machine, built at the expense of the French Government, was a
failure; Lilienthal and Pilcher were killed in experiments; and Chanute
and many others, from one cause or another, had relaxed their efforts,
though it subsequently became known that Professor Langley was still
secretly at work on a machine for the United States Government. The
public, discouraged by the failures and tragedies just witnessed,
considered flight beyond the reach of man, and classed its adherents
with the inventors of perpetual motion.

We began our active experiments at the close of this period, in October,
1900, at Kitty Hawk, North Carolina. Our machine was designed to be
flown as a kite, with a man on board, in winds from 15 to 20 miles an
hour. But, upon trial, it was found that much stronger winds were
required to lift it. Suitable winds not being plentiful, we found it
necessary, in order to test the new balancing system, to fly the machine
as a kite without a man on board, operating the levers through cords
from the ground. This did not give the practice anticipated, but it
inspired confidence in the new system of balance.

In the summer of 1901 we became personally acquainted with Mr. Chanute.
When he learned that we were interested in flying as a sport, and not
with any expectation of recovering the money we were expending on it, he
gave us much encouragement. At our invitation, he spent several weeks
with us at our camp at Kill Devil Hill, four miles south of Kitty Hawk,
during our experiments of that and the two succeeding years. He also
witnessed one flight of the power machine near Dayton, Ohio, in October,
1904.

The machine of 1901 was built with the shape of surface used by
Lilienthal, curved from front to rear like the segment of a parabola,
with a curvature 1/12 the depth of its cord; but to make doubly sure
that it would have sufficient lifting capacity when flown as a kite in
15 or 20-mile winds, we increased the area from 165 square feet, used in
1900, to 308 square feet--a size much larger than Lilienthal, Pilcher,
or Chanute had deemed safe. Upon trial, however, the lifting capacity
again fell very far short of calculation, so that the idea of securing
practice while flying as a kite had to be abandoned. Mr. Chanute, who
witnessed the experiments, told us that the trouble was not due to poor
construction of the machine. We saw only one other explanation--that the
tables of air-pressures in general use were incorrect.

[Illustration]

We then turned to gliding--coasting downhill on the air--as the only
method of getting the desired practice in balancing a machine. After
a few minutes' practice we were able to make glides of over 300 feet,
and in a few days were safely operating in 27-mile winds. In these
experiments we met with several unexpected phenomena. We found that,
contrary to the teachings of the books, the center of pressure on a
curved surface traveled backward when the surface was inclined, at small
angles, more and more edgewise to the wind. We also discovered that in
free flight, when the wing on one side of the machine was presented to
the wind at a greater angle than the one on the other side, the wing
with the greater angle descended, and the machine turned in a direction
just the reverse of what we were led to expect when flying the machine
as a kite. The larger angle gave more resistance to forward motion, and
reduced the speed of the wing on that side. The decrease in speed more
than counterbalanced the effect of the larger angle. The addition of a
fixed vertical vane in the rear increased the trouble, and made the
machine absolutely dangerous. It was some time before a remedy was
discovered. This consisted of movable rudders working in conjunction
with the twisting of the wings. The details of this arrangement are
given in specifications published several years ago.

The experiments of 1901 were far from encouraging. Although Mr. Chanute
assured us that, both in control and in weight carried per horse-power,
the results obtained were better than those of any of our predecessors,
yet we saw that the calculations upon which all flying machines had been
based were unreliable, and that all were simply groping in the dark.
Having set out with absolute faith in the existing scientific data, we
were driven to doubt one thing after another, till finally, after two
years of experiment, we cast it all aside, and decided to rely entirely
upon our own investigations. Truth and error were everywhere so
intimately mixed as to be undistinguishable. Nevertheless, the time
expended in preliminary study of books was not misspent, for they gave
us a good general understanding of the subject, and enabled us at the
outset to avoid effort in many directions in which results would have
been hopeless.

The standard measurements of wind-pressures is the force produced by a
current of air of one mile per hour velocity striking square against a
plane of one square foot area. The practical difficulties of obtaining
an exact measurement of this force have been great. The measurements by
different recognized authorities vary 50 per cent. When this simplest of
measurements presents so great difficulties, what shall be said of the
troubles encountered by those who attempt to find the pressure at each
angle as the plane is inclined more and more edgewise to the wind? In
the eighteenth century the French Academy prepared tables giving such
information, and at a later date the Aeronautical Society of Great
Britain made similar experiments. Many persons likewise published
measurements and formulas; but the results were so discordant that
Professor Langley undertook a new series of measurements, the results
of which form the basis of his celebrated work, "Experiments in
Aerodynamics." Yet a critical examination of the data upon which he
based his conclusions as to the pressures at small angles shows
results so various as to make many of his conclusions little better
than guesswork.

To work intelligently, one needs to know the effects of a multitude
of variations that could be incorporated in the surfaces of flying
machines. The pressures on squares are different from those on
rectangles, circles, triangles, or ellipses; arched surfaces differ
from planes, and vary among themselves according to the depth of
curvature; true arcs differ from parabolas, and the latter differ
among themselves; thick surfaces differ from thin, and surfaces
thicker in one place than another vary in pressure when the positions
of maximum thickness are different; some surfaces are most efficient
at one angle, others at other angles. The shape of the edge also makes
a difference, so that thousands of combinations are possible in so
simple a thing as a wing.

We had taken up aeronautics merely as a sport. We reluctantly entered
upon the scientific side of it. But we soon found the work so
fascinating that we were drawn into it deeper and deeper. Two testing
machines were built, which we believed would avoid the errors to which
the measurements of others had been subject. 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 50 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. A square plane, contrary to the measurements of all our
predecessors, gave a greater pressure at 30 degrees than at 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 tables, 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!

With accurate data for making calculations, and a system of balance
effective in winds as well as in calms, we were now in a position, we
thought, to build a successful power-flyer. The first designs provided
for a total weight of 600 lbs., including the operator and an eight
horse-power motor. But, upon completion, the motor gave more power than
had been estimated, and this allowed 150 lbs. to be added for
strengthening the wings and other parts.

Our tables made the designing of the wings an easy matter, and as
screw-propellers are simply wings traveling in a spiral course, we
anticipated no trouble from this source. We had thought of getting the
theory of the screw-propeller from the marine engineers, and then, by
applying our tables of air-pressures to their formulas, of designing
air-propellers suitable for our purpose. But so far as we could learn,
the marine engineers possessed only empirical formulas, 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
calculations alone. What at first seemed a 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.

[Illustration]

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 suitable propellers, with
proper diameter, pitch, and area of blade, to meet the requirements of
the flyer. 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.

The first flights with the power machine were made on December 17, 1903.
Only five persons besides ourselves were present. These were Messrs.
John T. Daniels, W. S. Dough, and A. D. Etheridge, of the Kill Devil
Life-Saving Station; Mr. W. C. Brinkley, of Manteo; and Mr. John Ward,
of Naghead. Although a general invitation had been extended to the
people living within five or six miles, not many were willing to face
the rigors of a cold December wind in order to see, as they no doubt
thought, another flying machine not fly. The first flight lasted only 12
seconds, a flight very modest compared with that of birds, but it was,
nevertheless, the first in the history of the world in which a machine
carrying a man had raised itself by its own power into the air in free
flight, had sailed forward on a level course without reduction of speed,
and had finally landed without being wrecked. The second and third
flights were a little longer, and the fourth lasted 59 seconds, covering
a distance of 852 feet over the ground against a 20-mile wind.

After the last flight the machine was carried back to camp and set down
in what was thought to be a safe place. But a few minutes later, while
we were engaged in conversation about the flights, a sudden gust of wind
struck the machine, and started to turn it over. All made a rush to stop
it, but we were too late. Mr. Daniels, a giant in stature and strength,
was lifted off his feet, and falling inside, between the surfaces, was
shaken about like a rattle in a box as the machine rolled over and over.
He finally fell out upon the sand with nothing worse than painful
bruises, but the damage to the machine caused a discontinuance of
experiments.

In the spring of 1904, through the kindness of Mr. Torrence Huffman, of
Dayton, Ohio, we were permitted to erect a shed, and to continue
experiments, on what is known as the Huffman Prairie, at Simms Station,
eight miles east of Dayton. The new machine was heavier and stronger,
but similar to the one flown at Kill Devil Hill. When it was ready for
its first trial every newspaper in Dayton was notified, and about a
dozen representatives of the Press were present. Our only request was
that no pictures be taken, and that the reports be unsensational, so as
not to attract crowds to our experiment grounds. There were probably 50
persons altogether on the ground. When preparations had been completed a
wind of only three or four miles 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 the next day, but were again
disappointed. The engine performed badly, and after a glide of only 60
feet, the machine 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 around 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-traveled thoroughfares, with electric cars passing every hour,
and seen by all the people living in the neighborhood for miles around,
and by several hundred others, yet these flights have been made by some
newspapers the subject of a great "mystery."

A practical flyer having been finally realized, we spent the years 1906
and 1907 in constructing new machines and in business negotiations. It
was not till May of this year that experiments (discontinued in October,
1905) were resumed at Kill Devil Hill, North Carolina. The recent
flights were made to test the ability of our machine to meet the
requirements of a contract with the United States Government to furnish
a flyer capable of carrying two men and sufficient fuel supplies for a
flight of 125 miles, with a speed of 40 miles an hour. The machine used
in these tests was the same one with which the flights were made at
Simms Station in 1905, though several changes had been made to meet
present requirements. The operator assumed a sitting position, instead
of lying prone, as in 1905, and a seat was added for a passenger. A
larger motor was installed, and radiators and gasoline reservoirs of
larger capacity replaced those previously used. No attempt was made to
make high or long flights.

In order to show the general reader the way in which the machine
operates, let us fancy ourselves ready for the start. The machine is
placed upon a single-rail track facing the wind, and is securely
fastened with a cable. The engine is put in motion, and the propellers
in the rear whir. You take your seat at the center of the machine beside
the operator. He slips the cable, and you shoot forward. An assistant
who has been holding the machine in balance on the rail starts forward
with you, but before you have gone 50 feet the speed is too great for
him, and he lets go. Before reaching the end of the track the operator
moves the front rudder, and the machine lifts from the rail like a kite
supported by the pressure of the air underneath it. The ground under you
is at first a perfect blur, but as you rise the objects become clearer.
At a height of 100 feet you feel hardly any motion at all, except for
the wind which strikes your face. If you did not take the precaution to
fasten your hat before starting, you have probably lost it by this
time. The operator moves a lever: the right wing rises, and the machine
swings about to the left. You make a very short turn, yet you do not
feel the sensation of being thrown from your seat, so often experienced
in automobile and railway travel. You find yourself facing toward the
point from which you started. The objects on the ground now seem to be
moving at much higher speed, though you perceive no change in the
pressure of the wind on your face. You know then that you are traveling
with the wind. When you near the starting-point the operator stops the
motor while still high in the air. The machine coasts down at an oblique
angle to the ground, and after sliding 50 or 100 feet, comes to rest.
Although the machine often lands when traveling at a speed of a mile a
minute, you feel no shock whatever, and cannot, in fact, tell the exact
moment at which it first touched the ground. The motor close beside you
kept up an almost deafening roar during the whole flight, yet in your
excitement you did not notice it till it stopped!

Our experiments have been conducted entirely at our own expense. In the
beginning we had no thought of recovering what we were expending, which
was not great, and was limited to what we could afford in recreation.
Later, when a successful flight had been made with a motor, we gave up
the business in which we were engaged, to devote our entire time and
capital to the development of a machine for practical uses. As soon as
our condition is such that constant attention to business is not
required, we expect to prepare for publication the results of our
laboratory experiments, which alone made an early solution of the flying
problem possible.



How We Made the First Flight

_By Orville Wright_


The flights of the 1902 glider had demonstrated the efficiency of our
system of maintaining equilibrium, and also the accuracy of the
laboratory work upon which the design of the glider was based. We then
felt that we were prepared to calculate in advance the performance of
machines with a degree of accuracy that had never been possible with the
data and tables possessed by our predecessors. Before leaving camp in
1902 we were already at work on the general design of a new machine
which we proposed to propel with a motor.

Immediately upon our return to Dayton, we wrote to a number of
automobile and motor builders, stating the purpose for which we desired
a motor, and asking whether they could furnish one that would develop
eight brake-horsepower, with a weight complete not exceeding 200 pounds.
Most of the companies answered that they were too busy with their
regular business to undertake the building of such a motor for us; but
one company replied that they had motors rated at 8 horse-power,
according to the French system of ratings, which weighed only 135
pounds, and that if we thought this motor would develop enough power for
our purpose they would be glad to sell us one. After an examination of
the particulars of this motor, from which we learned that it had but a
single cylinder of 4-inch bore and 5-inch stroke, we were afraid it was
much over-rated. Unless the motor would develop a full 8
brake-horsepower, it would be useless for our purpose.

Finally we decided to undertake the building of the motor ourselves. We
estimated that we could make one of four cylinders with 4-inch bore and
4-inch stroke, weighing not over two hundred pounds, including all
accessories. Our only experience up to that time in the building of
gasoline motors had been in the construction of an air-cooled motor,
5-inch bore and 7-inch stroke, which was used to run the machinery of
our small workshop. To be certain that four cylinders of the size we had
adopted (4" x 4") would develop the necessary 8 horse-power, we first
fitted them in a temporary frame of simple and cheap construction. In
just six weeks from the time the design was started, we had the motor on
the block testing its power. The ability to do this so quickly was
largely due to the enthusiastic and efficient services of Mr. C. E.
Taylor, who did all the machine work in our shop for the first as well
as the succeeding experimental machines. There was no provision for
lubricating either cylinders or bearings while this motor was running.
For that reason it was not possible to run it more than a minute or two
at a time. In these short tests the motor developed about nine
horse-power. We were then satisfied that, with proper lubrication and
better adjustments, a little more power could be expected. The
completion of the motor according to drawing was, therefore, proceeded
with at once.

[Illustration]

While Mr. Taylor was engaged with this work, Wilbur and I were busy in
completing the design of the machine itself. The preliminary tests of
the motor having convinced us that more than 8 horse-power would be
secured, we felt free to add enough weight to build a more substantial
machine than we had originally contemplated.

       *       *       *       *       *

For two reasons we decided to use two propellers. In the first place we
could, by the use of two propellers, secure a reaction against a greater
quantity of air, and at the same time use a larger pitch angle than was
possible with one propeller; and in the second place by having the
propellers turn in opposite directions, the gyroscopic action of one
would neutralize that of the other. The method we adopted of driving the
propellers in opposite directions by means of chains is now too well
known to need description here. We decided to place the motor to one
side of the man, so that in case of a plunge headfirst, the motor could
not fall upon him. In our gliding experiments we had had a number of
experiences in which we had landed upon one wing, but the crushing of
the wing had absorbed the shock, so that we were not uneasy about the
motor in case of a landing of that kind. To provide against the machine
rolling over forward in landing, we designed skids like sled runners,
extending out in front of the main surfaces. Otherwise the general
construction and operation of the machine was to be similar to that of
the 1902 glider.

When the motor was completed and tested, we found that it would develop
16 horse-power for a few seconds, but that the power rapidly dropped
till, at the end of a minute, it was only 12 horse-power. Ignorant of
what a motor of this size ought to develop, we were greatly pleased with
its performance. More experience showed us that we did not get one-half
of the power we should have had.

With 12 horse-power at our command, we considered that we could permit
the weight of the machine with operator to rise to 750 or 800 pounds,
and still have as much surplus power as we had originally allowed for in
the first estimate of 550 pounds.

Before leaving for our camp at Kitty Hawk we tested the chain drive for
the propellers in our shop at Dayton, and found it satisfactory. We
found, however, that our first propeller shafts, which were constructed
of heavy gauge steel tubing, were not strong enough to stand the shocks
received from a gasoline motor with light fly wheel, although they would
have been able to transmit three or four times the power uniformly
applied. We therefore built a new set of shafts of heavier tubing, which
we tested and thought to be abundantly strong.

We left Dayton, September 23, and arrived at our camp at Kill Devil Hill
on Friday, the 25th. We found there provisions and tools, which had been
shipped by freight several weeks in advance. The building, erected in
1901 and enlarged in 1902, was found to have been blown by a storm from
its foundation posts a few months previously. While we were awaiting the
arrival of the shipment of machinery and parts from Dayton, we were busy
putting the old building in repair, and erecting a new building to serve
as a workshop for assembling and housing the new machine.

Just as the building was being completed, the parts and material for the
machines arrived simultaneously with one of the worst storms that had
visited Kitty Hawk in years. The storm came on suddenly, blowing 30 to
40 miles an hour. It increased during the night, and the next day was
blowing over 75 miles an hour. In order to save the tar-paper roof, we
decided it would be necessary to get out in this wind and nail down more
securely certain parts that were especially exposed. When I ascended the
ladder and reached the edge of the roof, the wind caught under my large
coat, blew it up around my head and bound my arms till I was perfectly
helpless. Wilbur came to my assistance and held down my coat while I
tried to drive the nails. But the wind was so strong I could not guide
the hammer and succeeded in striking my fingers as often as the nails.

The next three weeks were spent in setting the motor-machine together.
On days with more favorable winds we gained additional experience in
handling a flyer by gliding with the 1902 machine, which we had found in
pretty fair condition in the old building, where we had left it the year
before.

Mr. Chanute and Dr. Spratt, who had been guests in our camp in 1901 and
1902, spent some time with us, but neither one was able to remain to see
the test of the motor-machine, on account of the delays caused by
trouble which developed in the propeller shafts.

While Mr. Chanute was with us, a good deal of time was spent in
discussion of the mathematical calculations upon which we had based our
machine. He informed us that, in designing machinery, about 20 per cent.
was usually allowed for the loss in the transmission of power. As we had
allowed only 5 per cent., a figure we had arrived at by some crude
measurements of the friction of one of the chains when carrying only a
very light load, we were much alarmed. More than the whole surplus in
power allowed in our calculations would, according to Mr. Chanute's
estimate, be consumed in friction in the driving chains. After Mr.
Chanute's departure, we suspended one of the drive chains over a
sprocket, hanging bags of sand on either side of the sprocket of a
weight approximately equal to the pull that would be exerted on the
chains when driving the propellers. By measuring the extra amount of
weight needed on one side to lift the weight on the other, we calculated
the loss in transmission. This indicated that the loss of power from
this source would be only 5 per cent., as we originally estimated. But
while we could see no serious error in this method of determining the
loss, we were very uneasy until we had a chance to run the propellers
with the motor to see whether we could get the estimated number of
turns.

The first run of the motor on the machine developed a flaw in one of the
propeller shafts which had not been discovered in the test at Dayton.
The shafts were sent at once to Dayton for repair, and were not received
again until November 20, having been gone two weeks. We immediately put
them in the machine and made another test. A new trouble developed. The
sprockets which were screwed on the shafts, and locked with nuts of
opposite thread, persisted in coming loose. After many futile attempts
to get them fast, we had to give it up for that day, and went to bed
much discouraged. However, after a night's rest, we got up the next
morning in better spirits and resolved to try again.

While in the bicycle business we had become well acquainted with the use
of hard tire cement for fastening tires on the rims. We had once used it
successfully in repairing a stop watch after several watchsmiths had
told us it could not be repaired. If tire cement was good for fastening
the hands on a stop watch, why should it not be good for fastening the
sprockets on the propeller shaft of a flying machine? We decided to try
it. We heated the shafts and sprockets, melted cement into the threads,
and screwed them together again. This trouble was over. The sprockets
stayed fast.

Just as the machine was ready for test bad weather set in. It had been
disagreeably cold for several weeks, so cold that we could scarcely work
on the machine for some days. But now we began to have rain and snow,
and a wind of 25 to 30 miles blew for several days from the north. While
we were being delayed by the weather we arranged a mechanism to measure
automatically the duration of a flight from the time the machine started
to move forward to the time it stopped, the distance traveled through
the air in that time, and the number of revolutions made by the motor
and propeller. A stop watch took the time; an anemometer measured the
air traveled through; and a counter took the number of revolutions made
by the propellers. The watch, anemometer and revolution counter were all
automatically started and stopped simultaneously. From data thus
obtained we expected to prove or disprove the accuracy of our propeller
calculations.

On November 28, while giving the motor a run indoors, we thought we
again saw something wrong with one of the propeller shafts. On stopping
the motor we discovered that one of the tubular shafts had cracked!

[Illustration]

Immediate preparation was made for returning to Dayton to build another
set of shafts. We decided to abandon the use of tubes, as they did not
afford enough spring to take up the shocks of premature or missed
explosions of the motor. Solid tool-steel shafts of smaller diameter
than the tubes previously used were decided upon. These would allow a
certain amount of spring. The tubular shafts were many times stronger
than would have been necessary to transmit the power of our motor if the
strains upon them had been uniform. But the large hollow shafts had no
spring in them to absorb the unequal strains.

Wilbur remained in camp while I went to get the new shafts. I did not
get back to camp again till Friday, the 11th of December. Saturday
afternoon the machine was again ready for trial, but the wind was so
light a start could not have been made from level ground with the run of
only sixty feet permitted by our monorail track. Nor was there enough
time before dark to take the machine to one of the hills, where, by
placing the track on a steep incline, sufficient speed could be secured
for starting in calm air.

Monday, December 14, was a beautiful day, but there was not enough wind
to enable a start to be made from the level ground about camp. We
therefore decided to attempt a flight from the side of the big Kill
Devil Hill. We had arranged with the members of the Kill Devil Hill Life
Saving Station, which was located a little over a mile from our camp, to
inform them when we were ready to make the first trial of the machine.
We were soon joined by J. T. Daniels, Robert Westcott, Thomas Beachem,
W. S. Dough and Uncle Benny O'Neal, of the station, who helped us get
the machine to the hill, a quarter mile away. We laid the track 150 feet
up the side of the hill on a 9-degree slope. With the slope of the
track, the thrust of the propellers and the machine starting directly
into the wind, we did not anticipate any trouble in getting up flying
speed on the 60-foot monorail track. But we did not feel certain the
operator could keep the machine balanced on the track.

When the machine had been fastened with a wire to the track, so that it
could not start until released by the operator, and the motor had been
run to make sure that it was in condition, we tossed up a coin to decide
who should have the first trial. Wilbur won. I took a position at one of
the wings, intending to help balance the machine as it ran down the
track. But when the restraining wire was slipped, the machine started
off so quickly I could stay with it only a few feet. After a 35 to
40-foot run it lifted from the rail. But it was allowed to turn up too
much. It climbed a few feet, stalled, and then settled to the ground
near the foot of the hill, 105 feet below. My stop watch showed that it
had been in the air just 3-1/2 seconds. In landing the left wing touched
first. The machine swung around, dug the skids into the sand and broke
one of them. Several other parts were also broken, but the damage to the
machine was not serious. While the test had shown nothing as to whether
the power of the motor was sufficient to keep the machine up, since the
landing was made many feet below the starting point, the experiment had
demonstrated that the method adopted for launching the machine was a
safe and practical one. On the whole, we were much pleased.

Two days were consumed in making repairs, and the machine was not ready
again till late in the afternoon of the 16th. While we had it out on the
track in front of the building, making the final adjustments, a stranger
came along. After looking at the machine a few seconds he inquired what
it was. When we told him it was a flying machine he asked whether we
intended to fly it. We said we did, as soon as we had a suitable wind.
He looked at it several minutes longer and then, wishing to be
courteous, remarked that it looked as if it would fly, if it had a
"suitable wind." We were much amused, for, no doubt, he had in mind the
recent 75-mile gale when he repeated our words, "a suitable wind!"

During the night of December 16, 1903, a strong cold wind blew from the
north. When we arose on the morning of the 17th, the puddles of water,
which had been standing about camp since the recent rains, were covered
with ice. The wind had a velocity of 10 to 12 meters per second (22 to
27 miles an hour). We thought it would die down before long, and so
remained indoors the early part of the morning. But when ten o'clock
arrived, and the wind was as brisk as ever, we decided that we had
better get the machine out and attempt a flight. We hung out the signal
for the men of the life saving station. We thought that by facing the
flyer into a strong wind, there ought to be no trouble in launching it
from the level ground about camp. We realized the difficulties of flying
in so high a wind, but estimated that the added dangers in flight would
be partly compensated for by the slower speed in landing.

We laid the track on a smooth stretch of ground about one hundred feet
north of the new building. The biting cold wind made work difficult, and
we had to warm up frequently in our living room, where we had a good
fire in an improvised stove made of a large carbide can. By the time all
was ready, J. T. Daniels, W. S. Dough and A. D. Etheridge, members of
the Kill Devil Life Saving Station; W. C. Brinkley, of Manteo, and
Johnny Moore, a boy from Nag's Head, had arrived.

We had a "Richards" hand anemometer with which we measured the velocity
of the wind. Measurements made just before starting the first flight
showed velocities of 11 to 12 meters per second, or 24 to 27 miles per
hour. Measurements made just before the last flight gave between 9 and
10 meters per second. One made just after showed a little over 8 meters.
The records of the Government Weather Bureau at Kitty Hawk gave the
velocity of the wind between the hours of 10:30 and 12 o'clock, the time
during which the four flights were made, as averaging 27 miles at the
time of the first flight and 24 miles at the time of the last.

       *       *       *       *       *

Wilbur, having used his turn in the unsuccessful attempt on the 14th,
the right to the first trial now belonged to me. After running the motor
a few minutes to heat it up, I released the wire that held the machine
to the track, and the machine started forward into the wind. Wilbur ran
at the side of the machine, holding the wing to balance it on the track.
Unlike the start on the 14th, made in a calm, the machine, facing a
27-mile wind, started very slowly. Wilbur was able to stay with it till
it lifted from the track after a forty-foot run. One of the life saving
men snapped the camera for us, taking a picture just as the machine had
reached the end of the track and had risen to a height of about two
feet. The slow forward speed of the machine over the ground is clearly
shown in the picture by Wilbur's attitude. He stayed along beside the
machine without any effort.

The course of the flight up and down was exceedingly erratic, partly due
to the irregularity of the air, and partly to lack of experience in
handling this machine. The control of the front rudder was difficult on
account of its being balanced too near the center. This gave it a
tendency to turn itself when started; so that it turned too far on one
side and then too far on the other. As a result the machine would rise
suddenly to about ten feet, and then as suddenly dart for the ground. A
sudden dart when a little over a hundred feet from the end of the track,
or a little over 120 feet from the point at which it rose into the air,
ended the flight. As the velocity of the wind was over 35 feet per
second and the speed of the machine against this wind ten feet per
second, the speed of the machine relative to the air was over 45 feet
per second, and the length of the flight was equivalent to a flight of
540 feet made in calm air. This flight lasted only 12 seconds, but it
was nevertheless the first in the history of the world in which a
machine carrying a man had raised itself by its own power into the air
in full flight, had sailed forward without reduction of speed, and had
finally landed at a point as high as that from which it started.

       *       *       *       *       *

At twenty minutes after eleven Wilbur started on the second flight. The
course of this flight was much like that of the first, very much up and
down. The speed over the ground was somewhat faster than that of the
first flight, due to the lesser wind. The duration of the flight was
less than a second longer than the first, but the distance covered was
about seventy-five feet greater.

Twenty minutes later the third flight started. This one was steadier
than the first one an hour before. I was proceeding along pretty well
when a sudden gust from the right lifted the machine up twelve to
fifteen feet and turned it up sidewise in an alarming manner. It began
sliding off to the left. I warped the wings to try to recover the
lateral balance and at the same time pointed the machine down to reach
the ground as quickly as possible. The lateral control was more
effective than I had imagined and before I reached the ground the right
wing was lower than the left and struck first. The time of this flight
was fifteen seconds and the distance over the ground a little over 200
feet.

Wilbur started the fourth and last flight at just 12 o'clock. The first
few hundred feet were up and down as before, but by the time three
hundred feet had been covered, the machine was under much better
control. The course for the next four or five hundred feet had but
little undulation. However, when out about eight hundred feet the
machine began pitching again, and, in one of its starts downward, struck
the ground. The distance over the ground was measured and found to be
852 feet; the time of the flight 59 seconds. The frame supporting the
front rudder was badly broken, but the main part of the machine was not
injured at all. We estimated that the machine could be put in condition
for flight again in a day or two.

While we were standing about discussing this last flight, a sudden
strong gust of wind struck the machine and began to turn it over.
Everybody made a rush for it. Wilbur, who was at one end, seized it in
front, Mr. Daniels and I, who were behind, tried to stop it by holding
to the rear uprights. All our efforts were vain. The machine rolled over
and over. Daniels, who had retained his grip, was carried along with it,
and was thrown about head over heels inside of the machine. Fortunately
he was not seriously injured, though badly bruised in falling about
against the motor, chain guides, etc. The ribs in the surfaces of the
machine were broken, the motor injured and the chain guides badly bent,
so that all possibility of further flights with it for that year were at
an end.

[Illustration]



Some Aeronautical Experiments

_By Wilbur Wright_


The difficulties 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 air at sufficient speed,
will not only sustain the weight of the wings themselves, but also that
of the engine, and of 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. As long ago as 1893 a machine weighing 8,000
lbs. demonstrated its power both to lift itself from the ground and to
maintain a speed of from 30 to 40 miles per hour; but it came to grief
in an accidental free flight, owing to the inability of the operators to
balance and steer it properly. This inability to balance and steer still
confronts students of the flying problem, although nearly ten years have
passed. 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
very considerable treatise. 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 recognized 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 try to imitate it. Now, there
are two ways of learning how 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 safest; 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.

       *       *       *       *       *

My own active interest in aeronautical problems dates back to the death
of Lilienthal in 1896. The brief notice of his death which appeared in
the telegraphic news at that time aroused a passive interest which had
existed from my childhood, and led me to take down from the shelves of
our home library a book on "Animal Mechanism," by Prof. Marey, which I
had already read several times. 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 18 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
pressures on curved surfaces, that a machine spreading 200 square feet
of wing surface would be sufficient for our purpose, and that places
could easily be found along the Atlantic coast where winds of 16 to 25
miles were not at all uncommon. When the winds were low it was our plan
to glide from the tops of sand hills, 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 plan 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 could 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 center 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 cross-piece of the
frame to the extreme front edge; (2) the encasing in the cloth of all
cross-pieces 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.

[Illustration]

With these plans we proceeded in the summer of 1900 to Kitty Hawk,
North Carolina, a little settlement located on the strip of land
that separates Albemarle Sound from the Atlantic Ocean. Owing to the
impossibility of obtaining suitable material for a 200-square-foot
machine, we were compelled to make it only 165 square feet in area,
which, according to the Lilienthal tables, would be supported at an
angle of three degrees in a wind of about 21 miles per hour. On the very
day that the machine was completed the wind blew from 25 to 30 miles per
hour, and we took it out for a trial as a kite. We found that while it
was supported with a man on it in a wind of about 25 miles, its angle
was much nearer 20 degrees than three degrees. Even in gusts of 30 miles
the angle of incidence did not get as low as three degrees, although the
wind at this speed has more than twice the lifting power of a 21-mile
wind. As winds of 30 miles per hour are not plentiful on clear days, it
was at once evident that our plan of practicing by the hour, day after
day, would have to be postponed. Our system of twisting the surfaces
to regulate the lateral balance was tried and found to be much more
effective than shifting the operator's body. On subsequent days, when
the wind was too light to support the machine with a man on it, we
tested it as a kite, working the rudders by cords reaching to the
ground. The results were very satisfactory, yet we were well aware that
this method of testing is never wholly convincing until the results are
confirmed by actual gliding experience.

We then turned our attention to making a series of actual measurements
of the lift and drift of the machine under various loads. So far as we
were aware, this had never previously been done with any full-size
machine. The results obtained were most astonishing, for 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 previously been
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 50 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. This deficiency
we supposed might be due to one or more of the following causes:--(1)
That the depth of the curvature of our surfaces was insufficient, being
only about one in 22, instead of one in 12. (2) That the cloth used in
our wings was not sufficiently air-tight. (3) That the Lilienthal tables
might themselves be somewhat in error. We decided to arrange our machine
for the following year so that the depth of the curvature of its
surfaces could be varied at will and its covering air-proofed.

Our attention was next turned to gliding, but no hill suitable for the
purpose could be found near our camp at Kitty Hawk. This compelled us to
take the machine to a point four miles south, where the Kill Devil sand
hill rises from the flat sand to a height of more than 100 feet. Its
main slope is toward the northeast, and has an inclination of 10
degrees. On the day of our arrival the wind blew about 25 miles an hour,
and as we had had no experience at all in gliding, we deemed it unsafe
to attempt to leave the ground. But on the day following, the wind
having subsided to 14 miles per hour, we made about a dozen glides. It
had been the original intention that the operator should run with the
machine to obtain initial velocity, and assume the horizontal position
only after the machine was in free flight. When it came time to land he
was to resume the upright position and alight on his feet, after the
style of previous gliding experiments. But in actual trial we found it
much better to employ the help of two assistants in starting, which the
peculiar form of our machine enabled us readily to do; and in landing we
found that it was entirely practicable to land while still reclining in
a horizontal position upon the machine. Although the landings were made
while moving at speeds of more than 20 miles an hour, neither machine
nor operator suffered any injury. The slope of the hill was 9.5 deg., or
a drop of one foot in six. We found that after attaining a speed of
about 25 to 30 miles with reference to the wind, or 10 to 15 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 deg., 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 center 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 that
employed in shifting the body of the operator of the machine.

When the time came to design our new machine for 1901 we decided to make
it exactly like the previous machine in theory and method of operation.
But as the former machine was not able to support the weight of the
operator when flown as a kite, except in very high winds and at very
large angles of incidence, we decided to increase its lifting power.
Accordingly, the curvature of the surfaces was increased to one in 12,
to conform to the shape on which Lilienthal's table was based, and to be
on the safe side we decided also to increase the area of the machine
from 165 square feet to 308 square feet, although so large a machine had
never before been deemed controllable. The Lilienthal machine had an
area of 151 square feet; that of Pilcher, 165 square feet; and the
Chanute double-decker, 134 square feet. As our system of control
consisted in a manipulation of the surfaces themselves instead of
shifting the operator's body, we hoped that the new machine would be
controllable, notwithstanding its great size. According to calculations,
it would obtain support in a wind of 17 miles per hour with an angle of
incidence of only three degrees.

[Illustration]

Our experience of the previous year having shown the necessity of a
suitable building for housing the machine, we erected a cheap frame
building, 16 feet wide, 25 feet long, and 7 feet high at the eaves. As
our machine was 22 feet wide, 14 feet long (including the rudder), and
about 6 feet high, it was not necessary to take the machine apart in any
way in order to house it. Both ends of the building, except the gable
parts, were made into doors which hinged above, so that when opened they
formed an awning at each end and left an entrance the full width of the
building. We went into camp about the middle of July, and were soon
joined by Mr. E. C. Huffaker, of Tennessee, an experienced aeronautical
investigator in the employ of Mr. Chanute, by whom his services were
kindly loaned, and by Dr. A. G. Spratt, of Pennsylvania, a young man who
has made some valuable investigations of the properties of variously
curved surfaces and the travel of the center of pressure thereon. Early
in August Mr. Chanute came down from Chicago to witness our experiments,
and spent a week in camp with us. These gentlemen, with my brother and
myself, formed our camping party, but in addition we had in many of our
experiments the valuable assistance of Mr. W. J. Tate and Mr. Dan Tate,
of Kitty Hawk.

       *       *       *       *       *

It had been our intention when building the machine to do most of the
experimenting in the following manner:--When the wind blew 17 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 10
glides in the time required for one in the other way. But when we came
to try it we found that a wind of 17 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 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 coefficient of .005 V^2 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 three degrees equals .545 of the pressure at 90 degrees is
too large, being nearly 50 per cent. greater than very recent
experiments of our own with a special 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.

[Illustration]

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. While our measurements differ considerably from
those of Lilienthal, 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. 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 lbs. 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
14 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 = 17 lbs., so that, although the
higher wind velocity must have caused an increase in the head
resistance, the tangential force still came within one pound 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 favorable 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 traveled in gliding with the vertical
fall, it was easily calculated that at a speed of 24 miles per hour the
total horizontal resistance 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 six 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. further 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
consumption 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 an 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 per hour with engines of
1,000 horse-power would still move four miles an hour even if the
engines were reduced to one 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.

[Illustration]

However, there is another way of flying which requires no artificial
motor, and many workers believe that success will first come 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 utilizing 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 six 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 two 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.

       *       *       *       *       *

[Illustration]

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-balanced surfaces is less at
angles of incidence of five degrees to 12 degrees than at an angle of
three degrees.

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

[Illustration]


  +------------------------------------------------------------------+
  |Transcriber's Note:                                               |
  |                                                                  |
  |                                                                  |
  |On page 15:                                                       |
  |                                                                  |
  |Wilbur, who was at one end, seized it in front, Mr. Daniels and I,|
  |who were behind, tried to stop it behind, tried to stop it by     |
  |holding to the rear uprights.                                     |
  |                                                                  |
  |has been changed to                                               |
  |                                                                  |
  |Wilbur, who was at one end, seized it in front, Mr. Daniels and I,|
  |who were behind, tried to stop it by holding to the rear uprights.|
  |                                                                  |
  |                                                                  |
  |On page 21:                                                       |
  |                                                                  |
  |Lilienthal was the first to discover this exceedingly though our  |
  |measurements differ considerably from those of Lilienthal. While  |
  |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, at Kitty|
  |Hawk we spent much time in measuring the horizontal pressure on   |
  |our unloaded machine at various angles of incidence.              |
  |                                                                  |
  |has been changed to                                               |
  |                                                                  |
  |While our measurements differ considerably from those of          |
  |Lilienthal, 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. At      |
  |Kitty Hawk we spent much time in measuring the horizontal         |
  |pressure on our unloaded machine at various angles of incidence.  |
  +------------------------------------------------------------------+





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