A model of the effects of pressure and crossflow velocity on composite propellant burning rate
- 18 June 1979
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Erosive burning of composite solid propellants - Experimental and modeling studiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Calculation of incompressible rough-wall boundary-layer flowsAIAA Journal, 1978
- Model for steady-state combustion of unimodal composite solid propellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Turbulent boundary layer with injection and surface roughnessAIAA Journal, 1977
- A model of erosive burning of composite propellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Heat transfer to the transpired turbulent boundary layerInternational Journal of Heat and Mass Transfer, 1972
- The combustion of solid monopropellants and composite propellantsSymposium (International) on Combustion, 1971
- Calculation of solid propellant burning rates from condensed-phase decomposition kineticsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- On Turbulent Flow Near a WallJournal of the Aeronautical Sciences, 1956