A finite element approach for prediction of aerothermal loads
- 12 May 1986
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- A Taylor-Galerkin finite element algorithm for transient nonlinear thermal-structural analysisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Finite element methods for high speed flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- A new finite element approach for prediction of aerothermal loads - Progress in inviscid flow computationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- The solution of non‐linear hyperbolic equation systems by the finite element methodInternational Journal for Numerical Methods in Fluids, 1984
- A study of flow separation in regions of shock wave-boundary layer interaction in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Numerical solutions of supersonic and hypersonic laminar flows over a two-dimensional compression cornerPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975