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aeroplanes-第5章

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In such a case it would now be over 5500 miles

from the center of the earth; and the centrifugal

pull would be decreased to such an extent that the

ball would go on and on until it came within the

sphere of influence from some other celestial

body。



EQUALIZING THE TWO MOTIONS。But now let us

assume that the line of flight is like that shown

at E; in Fig。 2; where it travels along parallel

with the surface of the earth。 In this case the

force of the ball equals the centripetal pull;or;

to put it differently; the centrifugal equals the

gravitational pull。



The constant tendency of the ball to fly off at

a tangent; and the equally powerful pull of

gravity acting against each other; produce a

motion which is like that of the earth; revolving

around the sun once every three hundred and

sixty…five days。



It is a curious thing that neither Langley; nor

any of the scientists; in treating of the matter of

flight; have taken into consideration this quality

of momentum; in their calculations of the elements

of flight。



_Fig。 2 Horizontal Flight_



All have treated the subject as though the

whole problem rested on the angle at which the

planes were placed。 At 45 degrees the lift and

drift are assumed to be equal。



LIFT AND DRIFT。The terms should be explained;

in view of the frequent allusion which

will be made to the terms hereinafter。 Lift

is the word employed to indicate the amount

which a plane surface will support while in flight。

Drift is the term used to indicate the resistance

which is offered to a plane moving forwardly

against the atmosphere。



_Fig。 3。 Lift and Drift_



In Fig。 3 the plane A is assumed to be moving

forwardly in the direction of the arrow B。 This

indicates the resistance。 The vertical arrow C

shows the direction of lift; which is the weight

held up by the plane。



NORMAL PRESSURE。Now there is another term

much used which needs explanation; and that is

normal pressure。 A pressure of this kind

against a plane is where the wind strikes it at

right angles。 This is illustrated in Fig。 4; in

which the plane is shown with the wind striking

it squarely。



It is obvious that the wind will exert a greater

force against a plane when at its normal。 On the

other hand; the least pressure against a plane is

when it is in a horizontal position; because then

the wind has no force against the surfaces; and

the only effect on the drift is that which takes

place when the wind strikes its forward edge。



_Fig。 4。 Normal Air Pressure_



_Fig。 5。 Edge Resistance_





HEAD RESISTANCE。Fig。 5 shows such a plane;

the only resistance being the thickness of the

plane as at A。 This is called head resistance;

and on this subject there has been much controversy;

and many theories; which will be considered

under the proper headings。



If a plane is placed at an angle of 45 degrees

the lift and the drift are the same; assumedly; because;

if we were to measure the power required

to drive it forwardly; it would be found to equal

the weight necessary to lift it。 That is; suppose

we should hold a plane at that angle with a heavy

wind blowing against it; and attach two pairs of

scales to the plane; both would show the same

pull。



_Fig。 6。 Measuring Lift and Drift_



MEASURING LIFT AND DRIFT。In Fig。 6; A is the

plane; B the horizontal line which attaches the

plane to a scale C; and D the line attaching it to

the scale E。 When the wind is of sufficient force

to hold up the plane; the scales will show the same

pull; neglecting; of course; the weight of the

plane itself。



PRESSURE AT DIFFERENT ANGLES。What every

one wants to know; and a subject on which a

great deal of experiment and time have been expended;

is to determine what the pressures are at

the different angles between the horizontal; and

laws have been formulated which enable the pressures

to be calculated。



DIFFERENCE BETWEEN LIFT AND DRIFT IN MOTION。The

first observation is directed to the differences

that exist between the lift and drift;

when the plane is placed at an angle of less than

45 degrees。 A machine weighing 1000 pounds

has always the same lift。 Its mass does not

change。 Remember; now; we allude to its mass;

or density。



We are not now referring to weight; because

that must be taken into consideration; in the

problem。 As heretofore stated; when an object

moves horizontally; it has less weight than when

at rest。 If it had the same weight it would not

move forwardly; but come to rest。



When in motion; therefore; while the lift; so

far as its mass is concerned; does not change; the

drift does decrease; or the forward pull is less

than when at 45 degrees; and the decrease is less

and less until the plane assumes a horizontal position;

where it is absolutely nil; if we do not consider

head resistance。



TABLES OF LIFT AND DRIFT。All tables of Lift

and Drift consider only the air pressures。 They

do not take into account the fact that momentum

takes an important part in the translation of an

object; like a flying machine。



A mass of material; weighing 1000 pounds while

at rest; sets up an enormous energy when moving

through the air at fifty; seventy…five; or one hundred

miles an hour。 At the latter speed the movement

is about 160 feet per second; a motion which

is nearly sufficient to maintain it in horizontal

flight; independently of any plane surface。



Such being the case; why take into account only

the angle of the plane? It is no wonder that

aviators have not been able to make the theoretical

considerations and the practical demonstrations

agree。



WHY TABLES OF LIFT AND DRIFT ARE WRONG。

A little reflection will show why such tables are

wrong。 They were prepared by using a plane

surface at rest; and forcing a blast of air against

the plane placed at different angles; and for determining

air pressures; this is; no doubt; correct。

But it does not represent actual flying conditions。

It does not show the conditions existing

in an aeroplane while in flight。



To determine this; short of actual experiments

with a machine in horizontal translation; is impossible;

unless it is done by taking into account

the factor due to momentum and the element

attributable to the lift of the plane itself due to its

impact against the atmosphere。



LANGLEY'S LAW。The law enunciated by

Langley is; that the greater the speed the less the

power required to propel it。 Water as a propelling

medium has over seven hundred times

more force than air。 A vessel having; for instance;

twenty horse power; and a speed of ten

miles per hour; would require four times that

power to drive it through the water at double the

speed。 The power is as the square of the speed。



With air the conditions are entirely different。

The boat submergence in the water is practically

the same; whether going ten or twenty miles a
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