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The Art of the Helicopter John Watkinson - Karatunov.net

The Art of the Helicopter John Watkinson - Karatunov.net

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

Fig. 3.1 (a) Lift is <strong>the</strong> reaction to <strong>the</strong> acceleration <strong>of</strong> air into a new direction. (b) <strong>The</strong> direction <strong>of</strong> acceleration<br />

<strong>of</strong> <strong>the</strong> air is derived as shown. <strong>The</strong> reaction must be in <strong>the</strong> opposite direction. (c) An increase in <strong>the</strong> angle <strong>of</strong><br />

attack increases <strong>the</strong> lift. (d) In <strong>the</strong> helicopter, lift is controlled through twisting <strong>the</strong> blade about a span-wise<br />

axis;a mechanism called fea<strong>the</strong>ring.<br />

allows <strong>the</strong>m to turn about a radial axis as can be seen in Figure 3.1(d). This mechanism<br />

is known as fea<strong>the</strong>ring.<br />

When <strong>the</strong> relative velocity alone is doubled with respect to <strong>the</strong> case in (b), <strong>the</strong> vector<br />

Va representing <strong>the</strong> change <strong>of</strong>velocity is doubled. As <strong>the</strong> air is moving twice as fast, <strong>the</strong><br />

wing accelerates <strong>the</strong> air in half<strong>the</strong> previous time. Achieving double <strong>the</strong> velocity in half<br />

<strong>the</strong> time means that <strong>the</strong> reaction is increased by a factor <strong>of</strong> four. In o<strong>the</strong>r words, <strong>the</strong><br />

reaction is proportional to <strong>the</strong> square <strong>of</strong><strong>the</strong> velocity. In practice four times as much lift<br />

would be quite unnecessary to balance <strong>the</strong> weight <strong>of</strong><strong>the</strong> machine and instead, as <strong>the</strong><br />

relative velocity doubled, <strong>the</strong> angle <strong>of</strong>attack would be reduced to about one-quarter<br />

<strong>of</strong> <strong>the</strong> previous value. This is <strong>the</strong> mechanism by which aircraft obtain <strong>the</strong> same lift over<br />

a range <strong>of</strong>airspeeds.

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