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The Art of the Helicopter John Watkinson - Karatunov.net

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

5.9<strong>The</strong> tail boom<br />

<strong>The</strong> tail boom must provide structural support for <strong>the</strong> tail rotor, <strong>the</strong> fin and <strong>the</strong> tail<br />

plane, as well as having some aerodynamic characteristics. Figure 5.13(a) shows that a<br />

tail boom which is a smooth continuation <strong>of</strong> <strong>the</strong> hull will have lower drag in forward<br />

flight than <strong>the</strong> ‘pod and boom’ construction shown at (b). However, a wide tail boom<br />

will suffer a greater download in <strong>the</strong> hover. Figure 5.13(c) shows that <strong>the</strong> tail boom <strong>of</strong>ten<br />

has a rounded rectangular shape to allow reasonable depth without excessive hover<br />

download.<br />

A streamlined tail boom may be practical on an executive transport, but for o<strong>the</strong>r<br />

purposes rear loading ramps or clamshell doors may be needed and <strong>the</strong>se always result<br />

in a hull having higher drag. <strong>The</strong> boom has to be high set and slim to give clearance<br />

for rear loading.<br />

<strong>The</strong> tail boom effectively couples two masses toge<strong>the</strong>r; <strong>the</strong> main rotor and <strong>the</strong> tail<br />

rotor. <strong>The</strong>se will each experience different forces, some static and some alternating. <strong>The</strong><br />

main rotor will apply vibrations to <strong>the</strong> hull, but <strong>the</strong> tail rotor will tend to lag behind<br />

because <strong>of</strong> its mass and <strong>the</strong> result will be stress on <strong>the</strong> tail boom. Figure 5.14(a) shows<br />

that when starting, whirling forces from <strong>the</strong> main rotor will rock <strong>the</strong> hull from side<br />

to side. A tail rotor mounted atop <strong>the</strong> tail fin will resist <strong>the</strong> rocking and place <strong>the</strong> tail<br />

boom in torsion. <strong>The</strong> mass <strong>of</strong> <strong>the</strong> tail and <strong>the</strong> torsional stiffness <strong>of</strong> <strong>the</strong> boom will create<br />

a resonant system and if <strong>the</strong> resonant frequency coincides with an exciting frequency<br />

<strong>the</strong> tail assembly will oscillate in torsion.<br />

If torsional oscillation results from a flight frequency, <strong>the</strong> resonant frequency will<br />

have to be changed. Intuitively, stiffening <strong>the</strong> tail boom would do this, but weakening<br />

it would also change <strong>the</strong> resonant frequency to a lower value. A lengthwise slot in <strong>the</strong><br />

Fig. 5.13 (a) A hull in which <strong>the</strong> tail boom is smoothly faired into <strong>the</strong> cabin will cause less drag in forward<br />

flight. (b) A pod-and-boom structure suffers from turbulence at <strong>the</strong> rear <strong>of</strong> <strong>the</strong> pod. (c) Tail boom cross-section<br />

which is deep but narrow gives strength without excessive download in <strong>the</strong> hover.

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