Handbook of structural stability
Buckling of curved plates and shells
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Author
Contributions
- Becker, Herbert, 1918- - Contributor
- United States. National Advisory Committee for Aeronautics - Contributor
Publication
1957 - National Advisory Committee for Aeronautics, Washington, D.C, District of Columbia
Language
English
Word Count
38,500 words, Guess
Page Count
154 pages
Identifiers
- ISBN-101680156284
- ISBN-139781680156287
- OCLC Control Number914328598
- Open LibraryOL44477653M
Classifications
- DDC623.817
- LCCTA645
Description
Available theories and test data on buckling of curved plates and shells are reviewed. For torsion and external-pressure loadings, the test data are correlated in terms of linear buckling theories for both the elastic and inelastic ranges. The cases which exhibit a marked disagreement between linear theory and test data include those of curved plates and cylinders under axial compression, cylinders under bending, and spherical plates under external pressure. These cases have been analyzed by a unified semiempirical approach for both the elastic and inelastic ranges which is satisfactory for analysis and design purposes. The effects of internal pressure on buckling of elements under uniaxial loads are discussed and data on various combined loadings are presented in interaction form.
Subjects
Series Statement
- Technical note / National Advisory Committee for Aeronautics -- 3783
- Technical note (United States. National Advisory Committee for Aeronautics) -- no. 3783.
Other Editions
- Handbook of structural stability
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