A numerical methodology coupling Navier-Stokes equations and structural modal equations for predicting 3-D transonic wing flutter is developed in this paper. A dual-time step implicit unfactored Gauss-Seidel iteration with the Roe scheme is employed for the flow solver. A modal approach is used for
✦ LIBER ✦
3D numerical simulation on fluid-structure interaction of structure subjected to underwater explosion with cavitation
✍ Scribed by Zhang, A-man; Ren, Shao-fei; Li, Qing; Li, Jia
- Book ID
- 118053529
- Publisher
- Springer
- Year
- 2012
- Tongue
- English
- Weight
- 923 KB
- Volume
- 33
- Category
- Article
- ISSN
- 0253-4827
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