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Tests on airplane fuselages, floats and hulls (1927)
NASA Technical Reports Server (NTRS) · leaf 17
7'- / 4 2^3 2 3 0° pitch and yaw S=. 2/60 sq.ft. 0° pitch and yaw S.1525sq.ft. V, f.p.s. 98.6 V, f.p.s. 98.6 DJb. 0.456 D, lb. 0.330 D/S, Ib./sq.ft. 2.111 D/S, Ib./sq.ft. 2.164 4.0 2.0 ■4.0 1.0 3.0 0.8 0.6ZZ ■0 1.0 0.8 -1.0 0° 4° 8" 12° 16° 0" 4" 8° 12° 16' Angle of pitch Angle of pitch Lift and…NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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