Pressure and velocity coupled response of composite solid propellants based upon a small perturbation of analysis
- 27 July 1981
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Response Function Theories That Account for Size Distribution Effects-A ReviewAIAA Journal, 1981
- On Statistical Analysis of Composite Solid Propellant CombustionAIAA Journal, 1974
- The calculation of turbulent boundary layers with foreign gas injectionInternational Journal of Heat and Mass Transfer, 1972
- A model of composite solid-propellant combustion based on multiple flamesAIAA Journal, 1970