Optimization analysis for axisymmetric rocket motor nozzle design based on assumptions for gas particle flow
Optimum thrust-nozzle contours for gas-particle flows.
01.10.1967
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Englisch
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
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