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)
Flight Dynamic Model of Aircraft Spinning
1990
56 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aeronautics , Aircraft , Spinning(Motion) , Angular motion , Balance , Coefficients , Computerized simulation , Data bases , Data processing , Data storage systems , Dynamics , Flight , Methodology , Mathematical models , Mathematical prediction , Moments , Oscillation , Recovery , Rotation , Steady state , Training aircraft , Trim(Aerodynamics) , Vortices , Stalling , Foreign technology , Spin recovery , Flight dynamics
Flight Dynamic Model of Aircraft Spinning
NTIS | 1990
|Engineering Index Backfile | 1954
|