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The Prediction of Helicopter Rotor Hover Performance using a ...

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0 0075<br />

00070<br />

00065<br />

00060<br />

Torque<br />

coefficient /<br />

solidity<br />

0 0055<br />

0-0O50<br />

00045<br />

x Flight tests (Ref 9)<br />

<strong>The</strong>ory<br />

<strong>The</strong>ory with correction for vertical drag<br />

0-075 O-O 80 0085 0-090<br />

Thrust coefficient/solidity<br />

0-095<br />

Fig.5 Wessex main rotor thrust and torque coefficients

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