Description of method by means of which, through simple layouts and calculations, mutual action of spars can be computed in functions of elasticity of different elements; these forces being known, it is very easy to establish more accurate calculation of spars and rationally determine stiffness that cross members should possess; analysis of torsion in wing of thick airfoil is necessary in order to make rational distribution of material between spars; practical calculations given.
Analysis of torsional stresses in airplane wings
Aviation Eng
Aviation Engineering ; 11 , n 6
1929
9 Figs.
Aufsatz (Zeitschrift)
Englisch
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