CHAPTER II.

SPEED AS A MEANS OF STABILITY.

It is recognized on all hands that speed is a great factor in the

problem of stability. To begin with, a machine going at high speed

would be practically untouched by gusts of wind, different densities

of air strata, holes in the air, etc. Also its greater momentum would

tend to keep it in a straight line, not only relative to its course

but also relative to itself. That is to say, its wings being started

in a horizontal plane, would tend to keep in the same plane and would

not easily tilt or sway out of it. Both these effects of natural law

show that a high speed machine must be more stable than a low speed

machine. How then are we to design a high speed machine?

Leaving aside the question of higher power, the first point that

suggests itself is to lessen the head resistance. All fast things,

boats, birds, arrows, even motor-cars, are made long and narrow. It

will be objected that a bird with its wings outspread is not long and

narrow, but in the sense in which this illustration is meant, the

bird’s wings, being merely its propelling apparatus, do not count, and

when the bird is at its fastest, as in the swoop of a hawk or an

eagle, the wings are shut tightly to the body so as to offer no

resistance to its lightning passage through the air. If we are to

follow previous experience in Nature’s laws, our aeroplanes must be

considerably reduced in span. To drive through the air at a high speed

with a machine of 40 foot span is a practical impossibility, both

because of the tremendous power it would require and also by reason of

the great strength the plane must have to withstand the resistance of

the air.

In reducing the span, however, we reduce the lifting surface of the

machine. But on the other hand it must be remembered that the lifting

efficiency is increased by increasing the speed. Lift is the product

of supporting surface and speed. A small plane driven at a high speed

will give as great a lift as a large plane driven at a low speed.

Speed, again, is the difference between the propelling power and the

head resistance, and we can increase the speed by decreasing the

resistance. It follows, then, that we need not necessarily give up

lifting power by reducing the span of the wings, since the shorter

span gives greater speed, and the increase of efficiency by reason of

the greater speed would go to make up for the loss of span.

It is, then, quite possible to design a short span machine which shall

be as efficient for lift as a long span machine, and which will have

the advantage of possessing, by reason of its speed, much greater

stability.

But the span is not the only factor in the speed problem. In the low

speed machines at present in use we have found it necessary to curve

the planes to get greater efficiency. This efficiency is also gained

at the expense of head resistance, and it is already recognized that

the higher the speed the less is the need of camber. This is the same

problem over again. A high speed flat plane will give as much lift as

a low speed cambered plane, and we gain in stability with every

additional mile per hour.

The third point to be considered in the problem of speed is the

resistance caused by the multitude of struts and wires, the body of

the pilot, the tanks, engine, and all the other impedimenta projecting

in all directions from the body of the aeroplane. It has occurred to

our builders that if the whole of these things could be collected

together and enclosed in a light covered-in car of a proper shape, the

skin friction of such a car would be much less than the total head

resistance offered by the different obstructions so covered. And there

is another advantage to be gained here, for if, at 40 miles per hour,

the force of the wind is very seriously uncomfortable for the pilot,

the position at such speeds as 70 or 100 miles per hour would be quite

impossible.

Natural Stability and the Parachute Principle in Aeroplanes · 第 2 / 6 章