Effect of normal pressure on the critical compressive stress of curved sheet
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Author
Contributions
- United States. National Advisory Committee for Aeronautics - Contributor
- Langley Aeronautical Laboratory - Contributor
Publication
1942 - National Advisory Committee for Aeronautics, Washington, D.C, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Identifiers
- ISBN-101680156349
- ISBN-139781680156348
- OCLC Control Number914330185
- Open LibraryOL44477664M
Classifications
- DDC551.54
- LCCQC885
Alternate Titles
- NACA Wartime Reports. Series L.
Description
Results are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal pressure at which buckles disappeared is independent of whether the buckles were made to disappear by increase of normal pressure or decrease of compressive stress.
Subjects
Series Statement
- Wartime Report / National Advisory Committee for Aeronautics -- no. L258
- Wartime Reports (United States. National Advisory Committee for Aeronautics) -- no. L258.
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