Supersonic rocket nozzle design for optimum thrust with chemically reacting gas flows
Optimum thrust nozzle contours for chemically reacting gas flows
1966-04-01
Report
No indication
English
General method for determining optimum thrust nozzle contours for chemically reacting gas flows
Engineering Index Backfile | 1967
|Optimum thrust-nozzle contours for gas-particle flows.
AIAA | 1967
|Optimum thrust-nozzle contours for gas-particle flows
AIAA | 1966
|