Mathematical theory of stability of fuselage subjected to torsional force in case of light-metal airplane in flight; experimental check of theory by testing india-rubber cylindrical shells of various thicknesses and lengths twisted by special apparatus.
Nature of torsional stability of monocoque fuselage
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 37 , n 269
1933
12 pages
Article (Journal)
English
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