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The Art of the Helicopter John Watkinson - Karatunov.net

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34 <strong>The</strong> <strong>Art</strong> <strong>of</strong> <strong>the</strong> <strong>Helicopter</strong><br />

Figure 2.12(b) shows that a solid object that moves against gas pressure increases<br />

<strong>the</strong> velocity <strong>of</strong> <strong>the</strong> rebounding molecules, whereas in (c) one moving with gas pressure<br />

reduces that velocity. <strong>The</strong> average velocity and <strong>the</strong> displacement <strong>of</strong> all <strong>the</strong> molecules<br />

in a layer <strong>of</strong> air near to a moving body is <strong>the</strong> same as <strong>the</strong> velocity and displacement<br />

<strong>of</strong> <strong>the</strong> body. Movement <strong>of</strong> a body results in a local increase, or decrease, in pressure.<br />

Thus sound is both a pressure and a velocity disturbance. Integration <strong>of</strong> <strong>the</strong> velocity<br />

disturbance gives <strong>the</strong> displacement.<br />

Despite <strong>the</strong> fact that a gas contains endlessly colliding molecules, a small mass or<br />

particle <strong>of</strong> gas can have stable characteristics if molecules leave and are replaced by<br />

o<strong>the</strong>rs having identical properties. As a result aerodynamics and acoustics seldom need<br />

to consider <strong>the</strong> molecular structure <strong>of</strong> air and <strong>the</strong> constant motion can be neglected.<br />

Thus when particle velocity and displacement is considered in aerodynamics or acoustics,<br />

this refers to <strong>the</strong> average values <strong>of</strong> a large number <strong>of</strong> molecules. In an undisturbed<br />

container <strong>of</strong> gas <strong>the</strong> particle velocity and displacement will both be zero everywhere.<br />

When <strong>the</strong> volume <strong>of</strong> a fixed mass <strong>of</strong> gas is reduced, <strong>the</strong> pressure rises. <strong>The</strong> gas acts<br />

like a spring; it is compliant. However, a gas also has mass. Sound travels through air<br />

by an interaction between <strong>the</strong> mass and <strong>the</strong> compliance. Imagine pushing a mass via<br />

a spring. It would not move immediately because <strong>the</strong> spring would have to be compressed<br />

in order to transmit a force. If a second mass were to be connected to <strong>the</strong> first<br />

by ano<strong>the</strong>r spring, it would start to move even later. Thus <strong>the</strong> speed <strong>of</strong> a disturbance<br />

in a mass/spring system depends on <strong>the</strong> mass and <strong>the</strong> stiffness. Sound travels through<br />

air without a <strong>net</strong> movement <strong>of</strong> <strong>the</strong> air.<br />

After <strong>the</strong> disturbance had propagated <strong>the</strong> masses would return to <strong>the</strong>ir rest position.<br />

<strong>The</strong> mass/spring analogy is helpful for a basic understanding, but is too simple to<br />

account for commonly encountered acoustic phenomena such as spherically expanding<br />

waves.<br />

Unlike solids, <strong>the</strong> elasticity <strong>of</strong> gas is a complicated process. If a fixed mass <strong>of</strong> gas is<br />

compressed, work has to be done on it. This will generate heat in <strong>the</strong> gas. If <strong>the</strong> heat<br />

is allowed to escape and <strong>the</strong> compression does not change <strong>the</strong> temperature, <strong>the</strong> process is<br />

said to be iso<strong>the</strong>rmal. However, if <strong>the</strong> heat cannot escape <strong>the</strong> temperature will rise and<br />

give a disproportionate increase in pressure. This process is said to be adiabatic and<br />

<strong>the</strong> Diesel engine depends upon it. In most acoustic cases <strong>the</strong>re is insufficient time for<br />

much heat transfer and so air is considered to act adiabatically. Figure 2.13 shows how<br />

<strong>the</strong> speed <strong>of</strong> sound c in air can be derived by calculating its elasticity under adiabatic<br />

conditions.<br />

Fig. 2.13 Calculating <strong>the</strong> speed <strong>of</strong> sound from <strong>the</strong> elasticity <strong>of</strong> air.

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