The effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion
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Author
Contributions
- Batdorf, S. B., author - Contributor
- Baab, George W., author - Contributor
- United States. National Advisory Committee for Aeronautics - Contributor
- Langley Aeronautical Laboratory - Contributor
Publication
1944 - National Advisory Committee for Aeronautics, Washington, D.C, District of Columbia
Language
English
Word Count
3,750 words, Guess
Page Count
15 pages
Identifiers
- ISBN-101680156365
- ISBN-139781680156362
- OCLC Control Number919146897
- Open LibraryOL44477774M
Classifications
- DDC621.4772
- LCCTA660.C9
Alternate Titles
- NACA Wartime Reports. Series L.
Description
The results of a series of tests to determine the effect of internal pressure on the buckling load of a thin cylinder under an applied torque indicated that internal pressure raises the shear buckling stress. The experimental results were analyzed with the aid of previously developed theory and a simple interaction formula was derived.
Subjects
Series Statement
- Wartime Report / National Advisory Committee for Aeronautics -- number L67
- Wartime Reports (United States. National Advisory Committee for Aeronautics) -- no. L67.
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