Experimental Investigation of the Partial- Admission Performance Characteristics of a Single-Stage Mach 2 Supersonic Turbine
1959
16 pages
Report
No indication
English
Jet & Gas Turbine Engines , Nozzle efficiency , Supersonic turbine , Admission , Characteristics , Efficiency , Nozzle , Partial , Performance , Pressure , Ratio , Rotor , Single , Specific , Stage , Static , Supersonic , Turbine , Work
Small, two-stage, partial-admission turbine
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