Critical combinations of torsion and direct axial stress for thin-walled cylinders

A theoretical solution is presented for the determination of the combinations of direct axial stress and torsion which cause thin-walled cylinders with either simply supported or clamped edges to buckle. This theoretical solution is used in conjunction with available test data to develop empirical c...

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Bibliographic Details
Main Author: Batdorf, S. B., (Author)
Corporate Author: Langley Aeronautical Laboratory.
Other Authors: Stein, Manuel., Schildcrout, Murry.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1345.
Subjects:
ISBN: 9781680156058
1680156055
Physical Description: 1 online resource (28, [8] pages) : illustrations, tables

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