k is the intent of this paper to study the geometrically nonlinear supersonic flutter characteristics of laminated composite thin-plate structures subjected to thermal loads. Interactive effects between the critical temperature difference and critical aerodynamic pressure for the plates are also stu
Nonlinear Viscoelastic Response of Unidirectional Polymeric Laminated Composite Plates Under Bending Loads
โ Scribed by S. R. Falahatgar; Manouchehr Salehi
- Publisher
- Springer Netherlands
- Year
- 2011
- Tongue
- English
- Weight
- 439 KB
- Volume
- 18
- Category
- Article
- ISSN
- 0929-189X
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