Critical Compressive Stress For Flat Rectangular Plates Supported Along All Edges And Elastically Restrained Against Rotation Among The Unloaded Edges
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Stresses Around Rectangular Cutouts in Torsion Boxes
A method is presented for calculating the stresses produced by rectangular cutouts of any size in torsion boxes. The problem is divided into a "box problem" and a "cover problem." The box problem is a special case of the general method of analyzing torsion boxes without cutouts. In the cover problem, simple shear-lag theory is used to obtain "key" stresses; the final distributions are obtained from these key stresses by means of simple rules or empirical distribution curves. Comparisons with the results from three series of tests in which the dimensions of the cutouts varied over a wide range are shown.
Annual Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1945
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.