In anticipation of an eventual VTOL requirement for civil aviation, NASA has been conducting studies directed toward determining and developing the technology required for a commercial VTOL transport. In this paper, the commercial transport configurations are briefly reviewed; the propulsion system specifications and components developed by the engine study contractor are presented and described; and methods for using the lift-propulsion system for aircraft attitude control are discussed
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
A design study was conducted for a remote lift-fan commercial V/STOL transport for the 1985 time per...
NASA research program on vertical and short takeoff and landing aircraft, including transports, heli...
A broad overview of the scope of research presently being supported by NASA in aircraft propulsion i...
Concept design is presented for two types of lift/cruise fan technology V/STOL aircraft, turbotip fa...
A simplified mission analysis was performed to determine an optimum engine cycle for a 100-passenger...
Wind tunnel test support, aircraft contractor support, a propulsion system computer card deck, preli...
Two types of lift/cruise fan technology aircraft were conceptually designed. One aircraft used turbo...
Technology flight vehicles were defined for three different approaches which demonstrate the concept...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
Conceptual design studies of V/STOL Lift Fan Commercial short-haul transport aircraft for the 1980-8...
Evaluation of air generator-remote lift fan propulsion system for VTOL transport
Technology associated with advanced conventional takeoff and landing transport aircraft is discussed...
The role of the Lewis Research Center in aeronautical propulsion is described. The state of the art ...
Propulsion requirements were determined for 0.5 and 0.7 Mach aircraft. Sensitivity studies were cond...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
A design study was conducted for a remote lift-fan commercial V/STOL transport for the 1985 time per...
NASA research program on vertical and short takeoff and landing aircraft, including transports, heli...
A broad overview of the scope of research presently being supported by NASA in aircraft propulsion i...
Concept design is presented for two types of lift/cruise fan technology V/STOL aircraft, turbotip fa...
A simplified mission analysis was performed to determine an optimum engine cycle for a 100-passenger...
Wind tunnel test support, aircraft contractor support, a propulsion system computer card deck, preli...
Two types of lift/cruise fan technology aircraft were conceptually designed. One aircraft used turbo...
Technology flight vehicles were defined for three different approaches which demonstrate the concept...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
Conceptual design studies of V/STOL Lift Fan Commercial short-haul transport aircraft for the 1980-8...
Evaluation of air generator-remote lift fan propulsion system for VTOL transport
Technology associated with advanced conventional takeoff and landing transport aircraft is discussed...
The role of the Lewis Research Center in aeronautical propulsion is described. The state of the art ...
Propulsion requirements were determined for 0.5 and 0.7 Mach aircraft. Sensitivity studies were cond...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
A design study was conducted for a remote lift-fan commercial V/STOL transport for the 1985 time per...
NASA research program on vertical and short takeoff and landing aircraft, including transports, heli...