Effects of small angle of attack on the radiating viscous shock layer solutions for Jovian entry
- 24 May 1978
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- An approximate inviscid radiating flow field analysis for outer planet entry probesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Numerical solution of the viscous hypersonic flow past blunted conesat angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Total radiative intensity calculations for 100% H2 and 87% H2-13% HeJournal of Quantitative Spectroscopy and Radiative Transfer, 1972
- The effect of viscosity in hypervelocity impact crateringPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- The Turbulent Boundary LayerPublished by Elsevier ,1956