Stability and Control of Helicopters in Steep Approaches. Volume IV. Derivatives and Transfer Functions for the AH-56A Compound Helicopter and Data on Low-Altitude Turbulence Representation.

摘要

Derivatives and transfer functions are presented for the Lockheed AH-56A helicopter. The flight conditions considered include airspeeds of from 0to 100knots and descent rates from 0to 28.8fps. A critical review is given of data on low altitude turbulence. (Author)