A thermomechanical buckling analysis ofmultilayered laminates with (across-the-width) strip delaminations is conducted on the basis of anisotropic thermoelasticity of the constituent layers and the Kirchhoff Love hypothesis of the classical laminate theory. With the assumption of generalized plane d
J integral for delaminated composite laminates
โ Scribed by L.J. Lee; D.W. Tu
- Publisher
- Elsevier Science
- Year
- 1993
- Tongue
- English
- Weight
- 603 KB
- Volume
- 47
- Category
- Article
- ISSN
- 0266-3538
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