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Monocoque Stability in Compression

Monocoque Stability in Compression IN R. & M. 1679 and AIRCRAFT ENGINEERING, December, 1935, the author gave certain expressions for the stable loads which a stiffenedskin panel, flat or curved, was capable of carrying without collapse by buckling. As regards the curved panel, it was there implicitly assumed that waving over relatively long lengths was impossible, because of the presence of rigid bulkheads or similar supports at intervals. While this will normally be the case in practice, it may happen that in some part of the structure a long length of panel remains without support other than that given to it by the ordinary frames and stringers. As this will tend to reduce the buckling load, it seems desirable to complete the theory to include the case of buckling in long waves. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

Monocoque Stability in Compression

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb030540
Publisher site
See Article on Publisher Site

Abstract

IN R. & M. 1679 and AIRCRAFT ENGINEERING, December, 1935, the author gave certain expressions for the stable loads which a stiffenedskin panel, flat or curved, was capable of carrying without collapse by buckling. As regards the curved panel, it was there implicitly assumed that waving over relatively long lengths was impossible, because of the presence of rigid bulkheads or similar supports at intervals. While this will normally be the case in practice, it may happen that in some part of the structure a long length of panel remains without support other than that given to it by the ordinary frames and stringers. As this will tend to reduce the buckling load, it seems desirable to complete the theory to include the case of buckling in long waves.

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: Sep 1, 1939

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