A flight dynamic model of aircraft spinning was developed. It is capable of simulating aircraft behavior 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.
Flight Dynamic Model of Aircraft Spinning
1990
45 pages
Report
No indication
English
Flight Dynamic Model of Aircraft Spinning
NTIS | 1990
|Engineering Index Backfile | 1954
|