Turbulent viscous shock layer solutions for Jovian entry at small angles of attack
- 16 January 1978
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Computational meshes for boundary layer problemsPublished by Springer Nature ,2008
- An approximate inviscid radiating flow field analysis for outer planet entry probesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Turbulent viscous-shock-layer solutions with strong vorticity interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Viscous-shock-layer solutions with radiation and ablation injection for Jovian entryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Numerical computation of two-dimensional viscous blunt body flows with an impinging shockPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Behavior of turbulent flow near a porous wall with pressure gradientAIAA Journal, 1970
- The effect of viscosity in hypervelocity impact crateringPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- The Turbulent Boundary LayerPublished by Elsevier ,1956