Finite element prediction of aerothermal-structural interaction of aerodynamically heated panels
- 8 June 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 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
- A finite element approach for prediction of aerothermal loadsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- A finite element approach for solution of the 3D Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Analysis of aerothermal loads on spherical dome protuberancesAIAA Journal, 1985