Critical combinations of longitudinal and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation
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Author
Contributions
- Stein, Manuel - Contributor
- Libove, Charles - Contributor
- Langley Aeronautical Laboratory - Contributor
- United States. National Advisory Committee for Aeronautics - Contributor
Publication
1946 - Langley Memorial Aeronautical Laboratory, Langley Field, VA, Virginia
Language
English
Word Count
3,500 words, Guess
Page Count
14 pages
Identifiers
- ISBN-101680156527
- ISBN-139781680156522
- OCLC Control Number857368708
- Open LibraryOL44477497M
Classifications
- DDC629.1341
- LCCTL671.2
Alternate Titles
- NACA wartime reports
Description
A theoretical investigation was made of the buckling of an infinitely long flat plate with edges elastically restrained against rotation under combinations of longitudinal and transverse direct stress. Interaction curves are presented that give the critical combinations of stress for several different degrees of elastic edge restraint, including simple support and complete fixity. It was found that an appreciable fraction of the critical longitudinal stress may be applied to the plate without any reduction in the transverse compressive stress required for buckling.
Subjects
Series Statement
- NACA collection
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