Artificial and Natural FlightMaxim, Hiram S. (Hiram Stevens)
Science
Artificial and Natural Flight
Maxim, Hiram S. (Hiram Stevens)
Aeronautics; Airplanes; Flight
CRYSTAL PALACE EXPERIMENTS.
Having fully satisfied myself that aeroplanes flying around a circle 200
feet in circumference had their lifting effect reduced to no
insignificant degree by constantly engaging air which had already had
imparted to it a downward movement by a previous revolution, I
determined to make some experiments where this trouble could not occur,
but the opportunity did not present itself until after the large
roundabout, erroneously described as “a captive flying machine,” was put
up at the Crystal Palace. This presented a fine opportunity for making
experiments at an extremely high velocity around a very large circle. I
will only refer to a few of these experiments. To a prolongation of one
of the long arms, I attached a thin steel wire rope about 60 feet above
the platform; I then attached to this wire rope the little device shown
(Fig. 39), in which _a_, is an aeroplane, 5 feet long and 1 foot wide,
placed at an inclination of 1 in 20. Great care was used in preparing
this aeroplane to see that it was free from blemish, smooth, and without
any irregularities. Both edges were sharp and the curvature was about
one-eighth of an inch on the underneath side. It was made relatively
thick in the middle where it was attached to the bar _c_, and thinner
at the ends. _b_, shows a lump of lead just heavy enough to balance the
bar _c_, and the tail; _d_, was a light but strong wooden frame, all the
edges being thin and sharp, and covered with a special silk that Mr.
Cody had found to be best for such purposes. The wire rope _e_, was
attached to the long arm which I referred to. The great length of the
bar _c_, and the accuracy with which the whole was made and balanced
caused the aeroplane to travel straight through the air adjusting itself
to all the shifting currents. Upon starting the machine on a very calm
day, this apparatus mounted as high as the point of support, sometimes
going 10 or more feet higher and sometimes 8 or 10 feet lower. However,
as a rule, it carried its own weight at a velocity of 80 miles an hour
around a circle 1,000 feet in circumference. Under these conditions, of
course, there could be no downward motion of the air as all the air
affected would be removed long before it could be struck the second time
by the aeroplane. I had no means of ascertaining exactly how much this
plane did actually lift, because the air was always moving to some
extent, and it was not an easy matter to ascertain whether it was above
or below the point of support. I am sure, however, that it was as much
as 36 lbs., or rather more than 7 lbs. to the square foot, and this is
just what it should have lifted, providing that we consider the results
obtained by smaller planes placed in an air blast of 40 miles an hour
and at the same angle. When these experiments were finished, I made a
very small apparatus having only about 25 square feet of lifting
surface, and this carried the weight of a man, in fact several gentlemen
Public-domain text, read in full here on John Shaqi.
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