국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	APPLICATION OF A PERFORMANCE MODELING TECHNIQUE TO AN AIRPLANE WITH VARIABLE SWEEP WINGS
저자	P. C. Redin
Keyword	Aircraft maneuvers; Aircraft performance; Computerized simulation; Drag; F-111 aircraft.
URL	http://www.dfrc.nasa.gov/DTRS/1981/PDF/H-1131.pdf
보고서번호	NASA-TP-1855
발행년도	1981
출처	NASA Dryden Flight Research Center
ABSTRACT	A performance modeling concept previously applied to an F-104F G and a YF-12C airplane was applied to an F-111A airplane. This application extended the concept to an airplane with variable sweep wings. The performance model adequately matched flight test data for maneuvers flown at different wing sweep angles at maximum afterburning and intermediate power settings. For maneuvers flown at less than intermediate power, including dynamic maneuvers, the performance model was not validated because the method used to correlate model and in-flight power setting was not adequate. Individual dynamic maneuvers were matched sucessfully by using adjustments unique to each maneuver.