Numerical Study of a Scramjet Engine Flowfield
- 1 September 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 20 (9) , 1182-1187
- https://doi.org/10.2514/3.51178
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Computational meshes for boundary layer problemsPublished by Springer Nature ,2008
- A parametric study of staged fuel injector configurations for scramjet applicationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Numerical study of a scramjet engine flow fieldPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Numerical investigation of the perpendicular injector flow field in a hydrogen fueled scramjetPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Critical influence of finite rate chemistry and unmixedness on ignition and combustion of supersonic H2-air streamsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- A numerical method for solving the Navier-Stokes equations with application to shock-boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975