SOME of the aerodynamic and mechanical problems of jet engines designed for supersonic flight speeds are discussed in this paper.The aerodynamic problems considered include the required range of operation of the compressor, the thermal efficiency of the cycle, the inlet-engine airflow match, and jet nozzle design. Structural difficulties due to high operating pressures and temperatures and the bearing and lube problems arising from high temperatures are also presented.
Turbojet-Engine Design Problems for Supersonic Flight
Sae Technical Papers
Pre-1964 SAE Technical Papers ; 1906
1954-01-01
Conference paper
English
Ramjet-Turbojet propulsion system for supersonic flight
Engineering Index Backfile | 1957
|Ramjet-Turbojet propulsion system for supersonic flight
Engineering Index Backfile | 1957
|Engineering Index Backfile | 1956
|THE RAMJET-TURBOJET PROPULSION SYSTEM FOR SUPERSONIC FLIGHT
SAE Technical Papers | 1957
|