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The Art of the Helicopter John Watkinson - Karatunov.net

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long. <strong>The</strong> cross-section <strong>of</strong> <strong>the</strong> duct matches <strong>the</strong> stream tube contraction as <strong>the</strong> fan is<br />

approached and so <strong>the</strong> reduced pressure caused by <strong>the</strong> fan is applied to <strong>the</strong> duct. As a<br />

result <strong>the</strong> effective area <strong>of</strong> <strong>the</strong> fenestron is <strong>the</strong> area <strong>of</strong> <strong>the</strong> duct mouth. <strong>The</strong> close fitting<br />

duct effectively prevents blade tip loss. <strong>The</strong> direction <strong>of</strong> rotation <strong>of</strong> <strong>the</strong> fenestron should<br />

be chosen on <strong>the</strong> same basis as that <strong>of</strong> a conventional tail rotor, namely <strong>the</strong> bottom<br />

blade going towards <strong>the</strong> nose.<br />

An advantage <strong>of</strong> <strong>the</strong> fenestron is that as it is set in <strong>the</strong> fin, <strong>the</strong>re can be no fin blockage<br />

as happens with a conventional tail rotor. In fact <strong>the</strong> fin is augmenting <strong>the</strong> effect <strong>of</strong><br />

<strong>the</strong> fan. <strong>The</strong> fenestron presents a much reduced hazard to ground personnel and is<br />

quieter. However, as <strong>the</strong> fenestron is inseparable from its duct assembly, a powerful<br />

fenestron can become quite large and ground clearance may be an issue. Some machines<br />

equipped with fenestrons have a sacrificial collapsing bumper intended to absorb <strong>the</strong><br />

energy <strong>of</strong> an unintended ground contact after which it must be replaced.<br />

5.11 NOTAR<br />

A helicopter without a tail rotor has a number <strong>of</strong> advantages. It can land in scrub<br />

without damage, ground personnel are less likely to be injured and <strong>the</strong>re may be a<br />

reduction in noise. <strong>The</strong> first attempt at a tail rotorless machine was <strong>the</strong> experimental<br />

Weir W-9, shown in Figure 5.17, that flew in <strong>the</strong> UK in 1944. This machine had a piston<br />

engine that, in addition to driving <strong>the</strong> main rotor, drove a variable pitch fan to blow air<br />

Fig. 5.17 <strong>The</strong> Weir W-9 had no tail rotor but instead ducted cooling air and exhaust gases down <strong>the</strong> tail boom<br />

to provide an anti-torque jet reaction. Twenty-five per cent <strong>of</strong> engine power was lost in <strong>the</strong> anti-torque system,<br />

which was not pursued.<br />

<strong>The</strong> tail 187

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