A Mathematical Model of a Single Main Rotor Helicopter for ... - Read
A Mathematical Model of a Single Main Rotor Helicopter for ... - Read
A Mathematical Model of a Single Main Rotor Helicopter for ... - Read
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APPENDIX E<br />
EMPENNAGE FORCES AND MOMENTS<br />
The expressions <strong>for</strong> the lift and drag coefficients <strong>for</strong> the vertical fin and the<br />
horizontal stabilizer are identical when referenced to a local wind-axes system <strong>for</strong><br />
the particular surface. (See appendix B.)<br />
The conditions at the stall <strong>of</strong> each surface are defined as follows:<br />
- cLM<br />
as - -<br />
a<br />
IT<br />
as = -<br />
4<br />
a1 = 1.2as<br />
as 1.<br />
IT<br />
IT<br />
as -<br />
4<br />
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