Performance characteristics and efficiency determined for air cooled turbojet engine suitable for supersonic speed flight
Experimental investigation of two-stage air-cooled turbine suitable for flight at Mach 2.5
1959-11-01
Report
No indication
English
An Experimental Single-stage Air-cooled Turbine
Emerald Group Publishing | 1953
|An Experimental Single-stage Air-cooled Turbine
Emerald Group Publishing | 1953
|