Compressive buckling of simply supported curved plates and cylinders of sandwich construction
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Author
Contributions
- Mayers, J. - Contributor
- United States. National Advisory Committee for Aeronautics - Contributor
Publication
1952 - National Advisory Committee for Aeronautics, Washington, D.C, Ohio
Language
English
Word Count
8,500 words, Guess
Page Count
34 pages
Identifiers
- ISBN-101680156233
- ISBN-139781680156232
- OCLC Control Number914328448
- Open LibraryOL44477649M
Classifications
- DDC624.17765
- LCCTA660.P6
Description
Theoretical solutions are presented for the buckling in uniform axial compression of two types of simply supported curved sandwich plates: the corrugated-core type and the isotropic type. Results are given in the form of equations and curves.
Subjects
Series Statement
- National Advisory Committee for Aeronautics -- no. 2601
- Technical note (United States. National Advisory Committee for Aeronautics) -- no. 2601.
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