Creep deformation and buckling of a circular cylindrical shell under axial compression
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Author
Publication
1967 - Flygtekniska försöksanstalten, Stockholm, Sweden
Language
English
Word Count
6,750 words, Guess
Page Count
27 pages
Identifiers
- Library of Congress Control Number72359802
- Open LibraryOL5372944M
Classifications
- DDC620.1/1283
- LCCTL507 .U45 no. 108
Subjects
Topics
Series Statement
- Aeronautical Research Institute of Sweden. Report
- 108
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