Stability and Control of Helicopters in Steep Approaches. Volume 4. Derivatives and Transfer Functions for the AH-56A Compound Helicopter and Data on Low-Altitude Turbulence Representation
MECHANICS RESEARCH INC LOS ANGELES CA
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Derivatives and transfer functions are presented for the Lockheed AH- 56A helicopter. The flight conditions considered include airspeeds of from 0 to 100 knots and descent rates from 0 to 28.8 fps. A critical review is given of data on low altitude turbulence.
- Military Aircraft Operations