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The Art of the Helicopter John Watkinson - Karatunov.net

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Technical background 51<br />

centripetal force in <strong>the</strong> absence <strong>of</strong> acceleration, a new virtual force <strong>of</strong> equal magnitude<br />

but opposite direction has to be imagined to act. This is called <strong>the</strong> centrifugal force. In<br />

<strong>the</strong> real world centrifugal force does not exist, it is a ma<strong>the</strong>matical convenience needed<br />

to allow an apparent state <strong>of</strong> equilibrium in a rotating frame <strong>of</strong> reference.<br />

In a fixed frame <strong>of</strong> reference, consider a turning rotor. Figure 2.31(b) shows that if<br />

one <strong>of</strong> <strong>the</strong> blades should move upwards, <strong>the</strong> centre <strong>of</strong> mass <strong>of</strong> <strong>the</strong> blade will move closer<br />

to <strong>the</strong> axis <strong>of</strong> rotation, reducing <strong>the</strong> moment <strong>of</strong> inertia. Conservation <strong>of</strong> momentum<br />

requires that <strong>the</strong> reduced moment <strong>of</strong> inertia be balanced by an increase in velocity.<br />

Consequently <strong>the</strong> blade will accelerate in <strong>the</strong> direction <strong>of</strong> rotation as it moves up. Naval<br />

gunners discovered a related effect which is that when a shell is fired a distance <strong>of</strong> several<br />

miles, <strong>the</strong> shell moves significantly with respect to <strong>the</strong> earth’s axis in a rotating frame<br />

<strong>of</strong> reference and so it will also experience conservation <strong>of</strong> momentum which takes it to<br />

<strong>the</strong> left or right <strong>of</strong> its intended target. <strong>The</strong>se are examples <strong>of</strong> <strong>the</strong> Coriolis effect, named<br />

after <strong>the</strong> ma<strong>the</strong>matician who derived <strong>the</strong> mechanics <strong>of</strong> rotating frames <strong>of</strong> reference.<br />

Figure 2.31(c) shows that when <strong>the</strong> frame <strong>of</strong> reference rotates at <strong>the</strong> same angular<br />

velocity as <strong>the</strong> component <strong>of</strong> interest, <strong>the</strong> rotation apparently disappears. However, <strong>the</strong><br />

conservation <strong>of</strong> momentum effect is still occurring and <strong>the</strong> blade appears to accelerate<br />

with respect to <strong>the</strong> frame <strong>of</strong> reference. In order to account for this acceleration, a new<br />

virtual force is imagined to act. This is called <strong>the</strong> Coriolis force. In <strong>the</strong> real world <strong>the</strong><br />

Coriolis force does not exist, like centrifugal force, it is a ma<strong>the</strong>matical convenience<br />

needed to allow <strong>the</strong> use <strong>of</strong> a rotating frame <strong>of</strong> reference.<br />

<strong>The</strong> uninformed will <strong>of</strong>ten make reference to both centrifugal and Coriolis forces as<br />

though <strong>the</strong>y really existed, usually as a result <strong>of</strong> reading an advanced textbook without<br />

understanding it. Such observations must be treated with suspicion. Centrifugal force<br />

and Coriolis force are <strong>the</strong> technical equivalent <strong>of</strong> <strong>the</strong> unicorn and <strong>the</strong> mermaid. <strong>The</strong>y<br />

are in <strong>the</strong> imagination and <strong>the</strong> literature but <strong>the</strong>y don’t exist.<br />

<strong>The</strong>re is a fur<strong>the</strong>r consequence <strong>of</strong> <strong>the</strong> use <strong>of</strong> a rotating frame <strong>of</strong> reference that affects<br />

vibration frequencies created in <strong>the</strong> rotor and transmitted to <strong>the</strong> hull. <strong>The</strong> frequencies<br />

generated in <strong>the</strong> rotor may have <strong>the</strong> rotational frequency <strong>of</strong> <strong>the</strong> rotor both added and<br />

subtracted. <strong>The</strong> phenomenon is known as heterodyning and was treated in section 2.11.<br />

2.16 Rotating masses and precession<br />

<strong>The</strong> rotors <strong>of</strong> a helicopter at flight RPM contain a large amount <strong>of</strong> stored energy and<br />

this alters <strong>the</strong> way <strong>the</strong>y respond to forces. In order to control <strong>the</strong> helicopter, <strong>the</strong> entire<br />

rotor has to be tilted in <strong>the</strong> direction <strong>the</strong> pilot wishes to go. This will not be achieved by<br />

applying a couple in that direction. Figure 2.32(a) shows that if one blade is considered,<br />

when a couple is applied to <strong>the</strong> rotor, as it rotates <strong>the</strong> couple will alternately try to move<br />

<strong>the</strong> blade up and down. In fact in a rotating frame <strong>of</strong> reference <strong>the</strong> blade experiences a<br />

sinusoidal forcing function at <strong>the</strong> rotational frequency <strong>of</strong> <strong>the</strong> rotor. <strong>The</strong> way in which<br />

<strong>the</strong> blade responds to this is non-intuitive.<br />

Figure 2.32(b) is drawn in a rotating frame <strong>of</strong> reference with respect to which <strong>the</strong><br />

blade is stationary and it becomes correct to refer to centrifugal force. <strong>The</strong> figure<br />

shows that if it is assumed that <strong>the</strong> blade is displaced from its normal plane <strong>of</strong> rotation<br />

and released, <strong>the</strong>re will be a component <strong>of</strong> centrifugal force trying to return <strong>the</strong> blade<br />

to <strong>the</strong> original plane. For small angles this force is proportional to <strong>the</strong> displacement,<br />

so <strong>the</strong> condition for SHM is met. <strong>The</strong> blade will oscillate like a pendulum about <strong>the</strong><br />

normal plane at some natural frequency. This frequency can be calculated from <strong>the</strong><br />

mass <strong>of</strong> <strong>the</strong> blade and <strong>the</strong> centrifugal force. It turns out that <strong>the</strong> frequency is nearly<br />

identical to <strong>the</strong> rotational frequency.

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