This paper is presented to solve the nonlinear dynamic buckling problem of a new type of composite cylindrical shells, made of ceram/metal functionally graded materials. The material properties vary smoothly through the shell thickness according to a power law distribution of the volume fraction of
โฆ LIBER โฆ
Dynamic response of an elastic cylindrical shell-solid core composite subject to time- dependent loading
โ Scribed by MCIVOR, I. K.; RUMINER, J. J.
- Book ID
- 120431069
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 1971
- Tongue
- English
- Weight
- 712 KB
- Volume
- 9
- Category
- Article
- ISSN
- 0001-1452
- DOI
- 10.2514/3.6455
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