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Two‐Spar Wing Stress Analysis: A Method Taking into Account the Finite Spacing of the Ribs, with Detailed Numerical Calculations and Test Results for a Model Wing Test Specimen

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 October 1949

Abstract

Notation. A cross‐section, plan and a perspective view of cell n are given in FIG. 4.

Citation

Goodey, W.J. (1949), "Two‐Spar Wing Stress Analysis: A Method Taking into Account the Finite Spacing of the Ribs, with Detailed Numerical Calculations and Test Results for a Model Wing Test Specimen", Aircraft Engineering and Aerospace Technology, Vol. 21 No. 10, pp. 313-319. https://doi.org/10.1108/eb031816

Publisher

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MCB UP Ltd

Copyright © 1949, MCB UP Limited