Approximations for hypervelocity nonequilibrium radiating, reacting,and conducting stagnation regions
- 1 October 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Thermophysics and Heat Transfer
- Vol. 3 (4) , 380-388
- https://doi.org/10.2514/3.28764
Abstract
No abstract availableKeywords
This publication has 21 references indexed in Scilit:
- A computational study of the flowfield surrounding the Aeroassist Flight Experiment vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Assessment of two-temperature kinetic model for ionizing airPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Navier-Stokes and viscous shock-layer solutions for radiating hypersonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Engineering Approximations for Radiating Nonequilibrium Shock LayersAIAA Journal, 1974
- Shock waves structured by nonequilibrium ionizing and thermal phenomenaPhysics of Fluids, 1973
- Radiating-Conducting Thick-Transparent Normal Shock SolutionPhysics of Fluids, 1972
- Radiative cooling and nonequilibrium chemistry coupling behind normal shock waves.AIAA Journal, 1972
- Radiative-gasdynamic coupling and nonequilibrium effect behind reflected shock wavesAIAA Journal, 1971
- Structure of Shock Waves with Nonequilibrium Radiation and IonizationPhysics of Fluids, 1969
- Ionization Rate of Air behind High-Speed Shock WavesPhysics of Fluids, 1966