Performance of a Variable Divergent-Shroud Ejector Nozzle Designed for Flight Mach Numbers Up to 3.0
1961
51 pages
Report
Keine Angabe
Englisch
Divergent nozzle , Pumping , Shrouded nozzle , Configuration , Divergence , Ejector , Fluid , Internal , Mechanics , Propulsion , Shroud , Simulation , System , Thrust , Turbojet , Variable
Internal-performance of two-position divergent shroud ejector
Engineering Index Backfile | 1961
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