A general method for determining optimum thrust nozzle contours for chemically reacting gas flows
2nd Propulsion Joint Specialist Conference ; 1966 ; Colorado Springs , CO , U.S.A.
01.01.1966
Aufsatz (Konferenz)
Elektronische Ressource
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
|