Optimization analysis for axisymmetric rocket motor nozzle design based on assumptions for gas particle flow
Optimum thrust-nozzle contours for gas-particle flows.
1967-10-01
Miscellaneous
No indication
English
Optimum thrust-nozzle contours for gas-particle flows.
AIAA | 1967
|Optimum thrust-nozzle contours for gas-particle flows
AIAA | 1966
|General method for determining optimum thrust nozzle contours for chemically reacting gas flows
Engineering Index Backfile | 1967
|