A conceptual design study is presented of 1,985 commercial tilt rotor STOL transports for a NASA 200 n. mi. (370 km) STOL Mission. A 100-passenger STOL Variant (Bell D313) of the Phase I VTOL Tilt Rotor Aircraft is defined. Aircraft characteristics are given; with the aircraft redesigned to meet 2,000-foot (610 m) field criteria, with emphasis on low fuel consumption and low direct operating cost. The 100-passenger STOL Tilt Rotor Aircraft was analyzed for performance, weights, economics, handling qualities, noise footprint and aeroelastic stability
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
A mathematical model for real-time flight simulation of a tilt rotor research aircraft was developed...
A design study was conducted for a remote lift-fan commercial V/STOL transport for the 1985 time per...
Aircraft were synthesized in the 21-, 45-, and 100- passenger categories. Technological factors were...
Results of conceptual engineering design studies of a STOL tilt rotor commercial aircraft for the 19...
The STOL substantiating data are presented of a conceptual design study of 1985 commercial tilt roto...
Conceptual design studies are summarized of tandem-rotor helicopter and tilt-rotor aircraft for a sh...
A preliminary design study was conducted to establish a minimum sized, low cost V/STOL tilt-rotor re...
The conceptual designs of four useful tilt-rotor aircraft for the 1975 to 1980 time period are prese...
The results of a study of folding tilt rotor (stowed rotor) aircraft are presented. The effects of d...
A conceptual design study was conducted to define a representative military and/or commercial tilt-p...
Results of conceptual design studies of tilt rotor and tandem helicopter aircraft for a 200 nautical...
Weight standardization, tilt and stopped rotor optimization, and noise sensitivity analysis of V/STO...
Conceptual design studies of pure and compound helicopter commercial short-haul transport aircraft f...
An investigation of three aircraft concepts, deflected slipstream STOL, helicopter VTOL, and fixed w...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
A mathematical model for real-time flight simulation of a tilt rotor research aircraft was developed...
A design study was conducted for a remote lift-fan commercial V/STOL transport for the 1985 time per...
Aircraft were synthesized in the 21-, 45-, and 100- passenger categories. Technological factors were...
Results of conceptual engineering design studies of a STOL tilt rotor commercial aircraft for the 19...
The STOL substantiating data are presented of a conceptual design study of 1985 commercial tilt roto...
Conceptual design studies are summarized of tandem-rotor helicopter and tilt-rotor aircraft for a sh...
A preliminary design study was conducted to establish a minimum sized, low cost V/STOL tilt-rotor re...
The conceptual designs of four useful tilt-rotor aircraft for the 1975 to 1980 time period are prese...
The results of a study of folding tilt rotor (stowed rotor) aircraft are presented. The effects of d...
A conceptual design study was conducted to define a representative military and/or commercial tilt-p...
Results of conceptual design studies of tilt rotor and tandem helicopter aircraft for a 200 nautical...
Weight standardization, tilt and stopped rotor optimization, and noise sensitivity analysis of V/STO...
Conceptual design studies of pure and compound helicopter commercial short-haul transport aircraft f...
An investigation of three aircraft concepts, deflected slipstream STOL, helicopter VTOL, and fixed w...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
A mathematical model for real-time flight simulation of a tilt rotor research aircraft was developed...
A design study was conducted for a remote lift-fan commercial V/STOL transport for the 1985 time per...