Current trends in military combat aircraft are clearly toward increased emphasis on multimission capability. This requires an engine that is considerably oversized when compared with the subsonic cruise or dash requirements of the aircraft. With oversized engines, engine performance is no longer an isolated element. A new approach is needed. This paper analyzes the inlet portion of the installed propulsion system. An assessment is made of the magnitude of the inlet drag associated with oversized engines for typical multimission aircraft. Some thoughts are presented on inclusion of inlet drag considerations into the engine cycle optimization process.
Inlet and Fan Aerodynamics
Sae Technical Papers
National Aeronautic and Space Engineering and Manufacturing Meeting ; 1968
01.02.1968
Aufsatz (Konferenz)
Englisch
Engineering Index Backfile | 1968
|Methodologies for Turbofan Inlet Aerodynamics Prediction
AIAA | 2017
|Inlet ground vortex aerodynamics under headwind conditions
Online Contents | 2011
|An Overview of Military Aircraft Supersonic Inlet Aerodynamics
British Library Conference Proceedings | 2012
|