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SemiMonocoque Cylinders

SemiMonocoque Cylinders IN the design of scmimonocoque aircraft structures it is generally assumed that, if failure occurs, it will take place by a collapse of the longitudinal stiffeners between the intermediate frames. This assumption has given reasonable results in the past and has undoubtedly been justified when applied to structures of small and medium size. It is well known that most of the intermediate frames in such structures are of minimum sizes, determined by practical considerations. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

SemiMonocoque Cylinders

Aircraft Engineering and Aerospace Technology , Volume 10 (6): 2 – Jun 1, 1938

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb030328
Publisher site
See Article on Publisher Site

Abstract

IN the design of scmimonocoque aircraft structures it is generally assumed that, if failure occurs, it will take place by a collapse of the longitudinal stiffeners between the intermediate frames. This assumption has given reasonable results in the past and has undoubtedly been justified when applied to structures of small and medium size. It is well known that most of the intermediate frames in such structures are of minimum sizes, determined by practical considerations.

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: Jun 1, 1938

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