Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 242
fiors to au/de StrapFig. 151. Aileron Hinge Fig. 152 STRESS ANALYSIS 148. Loading—The loading which is made the basis of an analysisshould be that given in the Government Specification for tail surfaces.The distribution of load between the fixed and movable surfaces isshown in Fig. 107. its…
Airplanes
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