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Volume 18, Issue 6
1 June 1946
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 18, Issue 6
Review Article| June 01 1946

Torsion in Conical and Cylindrical Shells Intersected by Planes

F.W. David, A.F.R.Ae.S.
F.W. David, A.F.R.Ae.S.
Mr. David is Chief Designer, Commonwealth Aircraft Corporation Pty. Ltd., Melbourne, Australia. The investigations recorded in these pages were completed in August, 1945.
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1946
Aircraft Engineering (1946) 18 (6): 200–205.
https://doi.org/10.1108/eb031381

STIFFENED conical and cylindrical shells discontinued by plane intersections not parallel to the plane of the applied torsional moment are quite frequently encountered in aircraft design. For example: cockpit enclosure trays and floors in fuselages, sloping frames and spars in wings, etc.

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© MCB UP Limited
1946
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