Supersonic rocket nozzle design for optimum thrust with chemically reacting gas flows
Optimum thrust nozzle contours for chemically reacting gas flows
01.04.1966
Report
Keine Angabe
Englisch
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
|