Computations of multispecies mixing between scramjet nozzle flow andhypersonic freestream
- 1 March 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 8 (2) , 500-506
- https://doi.org/10.2514/3.23504
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Computational design aspects of a NASP nozzle/afterbody experimentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Supercomputing of Supersonic Flows Using Upwind Relaxation and MacCormack SchemesJournal of Fluids Engineering, 1988
- Self-adaptive-grid method with application to airfoil flowAIAA Journal, 1987
- A detailed numerical model of a supersonic reacting mixing layerPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Numerical Simulation of Near Wakes Utilizing a Relaxation Turbulence ModelAIAA Journal, 1980
- The effect of viscosity in hypervelocity impact crateringPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969