A deflection formula for single-span beams of constant section subjected to combined axial and transverse loads
Description:
In this paper there is presented a deflection formula for single-span beams of constant section subjected to combined axial and transverse loads of the types commonly encountered in airplane design. The form of the equation is obtainable by dimensional analysis. Tables and curves of the non dimensional coefficients are appended to facilitate the use of the formula. The equation is applied to the determination of the spring constant of a beam. Tables and curves are presented to show the variatio…
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Date:
September 1935
Creator:
Burke, Walter F.
Partner:
UNT Libraries Government Documents Department