Current trends in military combat aircraft are towards increased emphasis on multi-mission capability which requires engine sizing at flight conditions other than those of basic missions, such as for short takeoff, for acceleration/climb capability in combat, or for supersonic capability; assessment is made of magnitude of inlet drag associated with oversized engines; paper attempts to simplify engine cycle by examining flow matching of inlet with initial component of augmented turbofan engine -- fan; flow requirements are established for fan and effects on performance and stability explored without regard to turbine and exhaust nozzle matching needs. (12319)
Inlet and fan aerodynamics
SAE Paper
SAE Meeting ; 1968 Inlets
1968
9 pages
Aufsatz (Konferenz)
Englisch
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