Lift, drag, and pitching moments of models modified according to moment-of-area rule were measured and compared with those of unmodified configuration at Mach number from 0.6 to 1.4 and at angles of attack from -- 2° to +12°.
Effect of moment-of-area-rule modifications of drag, lift, and pitching-moment characteristics of unswept aspect-ratio-6 wing and body combination
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 2-24-59A
1959
29 pages
Report
English
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