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TwoSpar Wing Stress Analysis

TwoSpar Wing Stress Analysis THE methods of wing stress analysis at present in use have in most cases been developed on the assumptions that the ribs are rigid in their own planes, and that they may be considered equivalent to an infinite number of infinitely thin ribs, infinitely closely spaced. The problem may then be treated by the methods of the calculus, as was done, for example, in an article by the writer in AIRCRAFT ENGINEERING, January and February, 1943. A more recent and much more comprehensive paper on the same subject has been published by J. HadjiArgyris and P. C. Dunne in the R. Ac. Society Journal, February, September and November, 1947, and May and June, 1949. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

TwoSpar Wing Stress Analysis

Goodey, W.J.
Aircraft Engineering and Aerospace Technology , Volume 21 (9): 15 – Sep 1, 1949
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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb031807
Publisher site
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Abstract

THE methods of wing stress analysis at present in use have in most cases been developed on the assumptions that the ribs are rigid in their own planes, and that they may be considered equivalent to an infinite number of infinitely thin ribs, infinitely closely spaced. The problem may then be treated by the methods of the calculus, as was done, for example, in an article by the writer in AIRCRAFT ENGINEERING, January and February, 1943. A more recent and much more comprehensive paper on the same subject has been published by J. HadjiArgyris and P. C. Dunne in the R. Ac. Society Journal, February, September and November, 1947, and May and June, 1949.

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: Sep 1, 1949

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