Multinozzle plume flow fields - Structure and numerical calculation
- 27 June 1977
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Three-dimensional supersonic internal flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- The numerical calculation of inviscid plume flow fieldsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- An analytic characteristic method for steady three-dimensional isentropic flowJournal of Fluid Mechanics, 1974
- Three-dimensional, supersonic, steady flows with any number of imbedded shocksPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- The Mach disc in underexpanded exhaust plumesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- The effect of viscosity in hypervelocity impact crateringPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969