Development and validation of a Navier-Stokes code for hypersonic external flow
- 1 March 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 27 (2), 160-166
- https://doi.org/10.2514/3.26120
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Toward a CFD nose-to-tail capability - Hypersonic unsteady Navier-Stokes code validationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Simulation of transonic viscous flow over a fighter-like configuration including inletPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Transonic Navier-Stokes solutions for a fighter-like configurationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Numerical simulation of unsteady, viscous, high-angle-of-attack flows using a partially flux-split algorithmPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Introductory aerothermodynamics of advanced space transportation systemsJournal of Spacecraft and Rockets, 1985
- A survey of aeroassisted orbit transferJournal of Spacecraft and Rockets, 1985
- Viscous real gas flowfields about three dimensional configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983