Various design concepts for a variable cycle engine applicable to a supersonic, mixed mission propulsion system which would combine the merits of a turbofan at subsonic operating conditions with those of a turbojet for supersonic operating conditions are briefly examined. In particular the integration of the variable area bypass injector with the core driven (aft fan block) fan stage is discussed and the technical benefits of the configuration are summarized.
VCE test bed engine for supersonic cruise research
1980-03-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Engine options for supersonic cruise aircraft
AIAA | 1978
|Engine options for supersonic cruise aircraft
Tema Archiv | 1978
|Supersonic Cruise Research 1979, part 2
NTRS | 1980
Supersonic Cruise Research 1979, part 1
NTRS | 1980
Fabrication research for supersonic cruise aircraft
Tema Archiv | 1979
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