Experimental Investigation of Two-Stage Air-Cooled Turbine Suitable for Flight at Mach 2.5
1959
53 pages
Report
No indication
English
Jet & Gas Turbine Engines , Air cooling , Performance characteristics , Supersonic speed , Turbojet engine , Air , Characteristics , Cooling , Efficiency , Effusion , Engine , Internal , Performance , Pressure , Range , Speed , Supersonic , Turbine , Turbojet
An Experimental Single-stage Air-cooled Turbine
Emerald Group Publishing | 1953
|An Experimental Single-stage Air-cooled Turbine
Emerald Group Publishing | 1953
|