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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Main Author: | |
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Corporate Author: | |
Other Authors: | , |
Format: | eBook |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947.
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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 |
Online Access:
Online Resources