The thrust, specific fuel consumption, and relative merits of the tandem fan and the dual reverse flow front fan propulsion systems for a supersonic V/STOL aircraft are discussed. Consideration is given to: fan pressure ratio, fan air burning, and variable core supercharging. The special propulsion system components required are described, namely: the reflecting front inlet/nozzle, the aft subsonic inlet, the reverse pitch fan, the variable core supercharger and the low pressure forward burner. The potential benefits for these unconventional systems are indicated.
Comparison of two parallel/series flow turbofan propulsion concepts for supersonic V/STOL
V/STOL Conference ; 1981 ; Palo Alto, CA
1981-12-01
Conference paper
No indication
English