A simple isoparametric assumed strain finite element formulation incorporating a third-order polynomial displacement model for the buckling and vibration analysis of initially stressed composite sandwich laminates is presented. The displacement model involves a nonlinear distribution of in-plane dis
Bond stresses in a randomly vibrating sandwich plate: Single mode theory
โ Scribed by D.J. Mead
- Publisher
- Elsevier Science
- Year
- 1964
- Tongue
- English
- Weight
- 849 KB
- Volume
- 1
- Category
- Article
- ISSN
- 0022-460X
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