Two‐Spar Wing Stress Analysis

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 June 1941


THE mathematically exact determination of the stress distribution in a two‐spar skin‐covered wing is, in the present state of knowledge, an impossibility, and is in fact quite unnecessary, since only a reasonable approximation is required. The theory outlined in this article will, it is hoped, give a reasonable approximation for a reasonable amount of work, while taking into account as many variables as possible.


Goodey, W. (1941), "Two‐Spar Wing Stress Analysis", Aircraft Engineering and Aerospace Technology, Vol. 13 No. 6, pp. 150-153.

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Copyright © 1941, MCB UP Limited

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