Pressure distributions in the form of differential pressure coefficients are presented for several wing chordwise and spanwise stations. Also presented are the results of limited analysis which show aircraft configuration effects, Mach number effects on the local wing loadings, comparisons of selected measured wing pressures with predicted pressures, and comparisons of wing loadings during right-turn and left-turn maneuvers. Differential pressure distributions for several maneuver flight conditions as function of aircraft configuration and flight Mach number; the variables are wingbody combinations, wing-fuselage stores, control surfaces, fuselage geometry, Mach number, flight maneuvers, wing load distribution, and wing profiles; 24 figures and 2 tables include numeric data.
Flight Measurements of Lifting Pressures for a Thin Low-Aspect-Ratio Wing at Subsonic, Transonic, and Low Supersonic Speeds
1977
120 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft , Low aspect ratio wings , Pressure distribution , Flight tests , Mach number , Aerodynamic loads , Aircraft maneuvers , Subsonic speed , Transonic flight , Wing span , Aerodynamic coefficients , Body-wing configurations , Control surfaces , Wing loading , Wing profiles , Wing-fuselage stores
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