Aeronautics; Aeronautics, Military; World War, 1914-1918 -- Aerial operations
The problems of starting and landing the airplane have been many. The
early Wright machine had to run on a little trolley down a track in
order to gain sufficient momentum to take to the air. Later machines
showed an improvement on this. Henry Farman attached wooden skids to the
bottom of his airplane and fastened wheels to them by means of heavy
rubber bands. Thus he could start his motor and run over the ground
until his speed permitted him to rise, while in making a descent the
wheels flew back on their flexible bands and the stout skids absorbed
the shock of the fall. Most of the modern machines have a wheeled
framework below the fuselage, which permits them to run over the ground
in starting and also in making a descent. The danger of engine failure
becomes very important when near to the ground, as the pilot has no time
to get his machine into a gradual glide and avoid a bad accident. This
danger is sometimes averted by installing two engines, so that if one
stops the other will carry the airplane on up into the air and prevent a
smash-up. But the thing which has greatest effect on the ability of the
airplane to land easily is its own design and speed. The wings of the
airplane, its propeller and its whole construction have been planned so
that it can support itself best in the air when flying at a certain
fixed speed. Suppose this speed for a certain type of airplane to be 150
miles per hour. The airplane cannot land while traveling at that rate,
yet its speed while still in the air can only be diminished to a certain
point with safety, and below that point it may not be able to sustain
itself in flight. The pilot must be able to land his machine without
accident and without throttling his engine below this danger line; while
the designer of airplanes must struggle to produce a machine which,
while flying best at its maximum speed, will _fly_ at a much lower rate
of motion, when necessary to effect a landing.
The supporting power of the wings depends partly on their size and
partly on their rate of motion. Small wings moving at high speed produce
the same supporting pressure of air beneath them as large wings flying
at slow speed. The problem of a safe landing could best be solved by
building wings whose area could be altered in mid-air. When traveling
under full power the pilot would reduce the wing spread, as the smaller
wings would then be sufficient to support the weight of the machine and
would create less air resistance. When about to land, he would increase
the spread of the wings, so that at the slower rate of motion through
the air he might take advantage of a larger supporting surface. Nothing
of this sort has yet been worked out on a practical scale, but many have
been the suggestions for "telescoping wings."
Public-domain text, read in full here on John Shaqi.
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