Analysis of results obtained in systematic research program concerned with effects of wing sweep, aspect ratio, taper ratio, and dihedral on rolling moment due to sideslip of wing-fuselage configurations up to Mach numbers of about 0.95; new methods and design charts for estimating effects of compressibility and wing geometry on rolling moment due to sideslip.
Rolling moment due to sideslip of swept wings at subsonic and transonic speeds
NASA -- Tech Note
1960
81 pages
Report
English
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Rolling and yawing moments for swept-back wings in sideslip at supersonic speeds
Engineering Index Backfile | 1951
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