The modern fan engine has a propeller-like component whose aerodynamic performance differs from that of a propeller at the blade level but serves the same function. The blading aerodynamics differs from that of a compressorCompressor in notable ways.
Bypass and Other Engines
The Vortex and The Jet ; Kapitel : 11 ; 121-124
2022-02-25
4 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Individual bypass throttling in fighter engines
AIAA | 1982
|Principles and Applications of Bypass Turbojet Engines
SAE Technical Papers | 1956
|Improving Performance Retention of High Bypass Engines
SAE Technical Papers | 1975
|Advanced fan development for high bypass engines
AIAA | 1968
|