Optimization analysis for axisymmetric rocket motor nozzle design based on assumptions for gas particle flow
A general method for determining optimum thrust nozzle contours for gas-particle flows.
01.06.1966
Aufsatz (Konferenz)
Keine Angabe
Englisch
Optimum thrust-nozzle contours for gas-particle flows.
AIAA | 1967
|Optimum thrust-nozzle contours for gas-particle flows
AIAA | 1966
|Optimum thrust-nozzle contours for gas-particle flows.
NTRS | 1967
|General method for determining optimum thrust nozzle contours for chemically reacting gas flows
Engineering Index Backfile | 1967
|