Stresses Produced in Airplane Wings by Gusts (1932)
NASA Technical Reports Server (NTRS) · leaf 45
Figs.17,18 H.A.C.A. Technical Memorandum No.654 Stat, deflection Time,m in. Pig.17 Deflection y of F 13 starboard wing(8.85 m (29.04 ft.) from fuselage center) during fliglat. Gross weight = 1.8 t (3968.3 lb.) V = 130 km/h (80.8 mi./hr.) … 0 2 4 6 Time, s Pig. 18 Deflection y of P 13 starboard wing in gasts. 8.85 m (29»04 ft.) from center of fuselage. Gross weight =1.8 t (3968.3 Ih.) V = 130 km/h (80.8 mi./hr.).
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