Computational aerothermodynamic design issues for hypersonic vehicles
- 23 June 1997
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 100 references indexed in Scilit:
- Data-parallel lower-upper relaxation method for reacting flowsAIAA Journal, 1994
- Examination of theory for bow shock ultraviolet rocket experiments. IJournal of Thermophysics and Heat Transfer, 1994
- Review of chemical-kinetic problems of future NASA missions. II - Mars entriesJournal of Thermophysics and Heat Transfer, 1994
- Design of a wing shape for study of hypersonic crossflow transition in flightComputing Systems in Engineering, 1992
- Computation of laminar hypersonic compression-corner flowsAIAA Journal, 1991
- Numerical study of chemically reacting flows using a lower-upper symmetric successive overrelaxation schemeAIAA Journal, 1989
- Lower-upper Symmetric-Gauss-Seidel method for the Euler and Navier-Stokes equationsAIAA Journal, 1988
- Composite grid generation code for general 3-D regions - The EAGLE codeAIAA Journal, 1988
- Separated flow treatment with a new turbulence modelAIAA Journal, 1986
- A Finite-Difference Method for Calculating Compressible Laminar and Turbulent Boundary LayersJournal of Basic Engineering, 1970