A detailed investigation of flight buffeting response of an F-111A aircraft was performed. AIAA Paper No. 74-358 presented results of an initial study of wing and fuselage responses measured at subsonic speeds and wing leading-edge sweep of 26 degrees. The present paper gives additional results for wing sweeps of 26, 50 and 72.5 degrees at Mach numbers up to 1.2 including horizontal tail responses. Power spectra, response time histories, variations of rms response with angle of attack, and effects of Mach number and wing sweep angle are discussed.
Update on an investigation of flight buffeting of a variable-sweep aircraft
American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting ; 1975 ; Pasadena, CA
1975-01-01
Conference paper
No indication
English
Flight testing of variable sweep wing aircraft
Engineering Index Backfile | 1963
|AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Buffeting Flows over a Low-Sweep Delta Wing
Online Contents | 2004
|Buffeting flows over a low-sweep delta wing
Tema Archive | 2004
|Flight Testing of a Variable Sweep Wing Aircraft
NTIS | 1963
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