Critical combinations of torsion and direct axial stress for thin-walled cylinders
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Author
Contributions
- Stein, Manuel - Contributor
- Schildcrout, Murry - Contributor
- United States. National Advisory Committee for Aeronautics - Contributor
- Langley Aeronautical Laboratory - Contributor
Publication
1947 - National Advisory Committee for Aeronautics, Washington, D.C, District of Columbia
Language
English
Word Count
7,000 words, Guess
Page Count
28 pages
Identifiers
- ISBN-101680156055
- ISBN-139781680156058
- OCLC Control Number914248233
- Open LibraryOL44477640M
Classifications
- DDC624.17762
- LCCTA660.S5
Description
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 curves and formulas for use in design. Comparisons are made with theoretical and empirical solutions obtained in other investigations.
Subjects
Series Statement
- National Advisory Committee for Aeronautics technical note -- no. 1345
- Technical note (United States. National Advisory Committee for Aeronautics) -- no. 1345.
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