A new finite element approach for prediction of aerothermal loads - Progress in inviscid flow computations
- 15 July 1985
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- The solution of non‐linear hyperbolic equation systems by the finite element methodInternational Journal for Numerical Methods in Fluids, 1984
- The use of domain splitting with an explicit hyperbolic solverComputer Methods in Applied Mechanics and Engineering, 1984
- Solution of the Euler equations for complex configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Finite element formulations for convection dominated flows with particular emphasis on the compressible Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Capability for aerothermal-structural tests of large-to-full-scale components of future space transportation systemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- A detached shock calculation by second-order finite differencesJournal of Computational Physics, 1967