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Compressive buckling of simply supported curved plates and cylinders of sandwich construction /
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.
| Call Number: | Libro Electrónico |
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| Format: | Electronic eBook |
| Language: | Inglés |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1952.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 2601. |
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| Online Access: | Texto completo |