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Volume 21, Issue 10
1 October 1949
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 21, Issue 10
Review Article| October 01 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 Available to Purchase

W.J. Goodey
W.J. Goodey
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1949
Aircraft Engineering (1949) 21 (10): 313–319.
https://doi.org/10.1108/eb031816

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

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© MCB UP Limited
1949
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