摘要: A flight dynamic model of aircraft spinning been developed. It is capable of simulating aircraft behaviour from conventional flight through stall, spin entry, steady spin, and spin recovery. A data base storage technique has been ... 展开 A flight dynamic model of aircraft spinning been developed. It is capable of simulating aircraft behaviour from conventional flight through stall, spin entry, steady spin, and spin recovery. A data base storage technique has been used to provide the six force and moment coefficients required. The data base embodies rotary balance data measured for a basic training aircraft plus computed small disturbance data calculated from a line vortex model. Keywords: Training aircraft; Spinning motion; Trim aerodynamics; Angular motion; Mathematical predication; Computerized simulation; Vortices/oscillation; Australia. (EDC) 收起