Supersonic flutter analysis of laminated composite circular cylindrical shells is investigated by using an axisymmetric shell finite element based on the field-consistency approach. The formulation includes transverse shear deformation and in-plane and rotary inertia effects. The aerodynamic force i
Finite element method applied to the supersonic flutter of circular cylindrical shells
β Scribed by Maher N. Bismarck-Nasr
- Publisher
- John Wiley and Sons
- Year
- 1976
- Tongue
- English
- Weight
- 450 KB
- Volume
- 10
- Category
- Article
- ISSN
- 0029-5981
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