The patent application relates to an invention that pertains to lifting and propulsion systems in vertical and short takeoff and landing type aircraft. More particularly, this invention pertains to such systems wherein the power source is a bypass turbofan engine and where remote lifting fans are powered by turbojet exhaust while bypass fan efflux is vectored to provide lift or thrust.
Fan Lift-Cruise V/STOL Aircraft
1976
13 pages
Report
No indication
English
The lift/cruise fan multimission V/STOL aircraft
AIAA | 1975
|Review of V/STOL lift/cruise fan technology
NTRS | 1976
|Effect of Exhaust Deflectors on the Design of Lift Plus Lift/Cruise V/STOL Aircraft
SAE Technical Papers | 1973
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