Add to ORKGResults of conceptual engineering design studies of a STOL tilt rotor commercial aircraft for the 1985 time frame are presented. The details of aircraft size, performance, flying qualities, noise, and cost are included. The savings in terms of fuel economy resulting from STOL operations compared with VTOL vehicles are determined
The performances of a derivative concept of a 1985 STOL tilt rotor transport, and of a second concep...
A design study was conducted for a remote lift-fan commercial V/STOL transport for the 1985 time per...
Evaluation of advanced VTOL, STOL, and conventional takeoff and landing aircraft for short haul tran...
A conceptual design study is presented of 1,985 commercial tilt rotor STOL transports for a NASA 200...
Aircraft were synthesized in the 21-, 45-, and 100- passenger categories. Technological factors were...
The STOL substantiating data are presented of a conceptual design study of 1985 commercial tilt roto...
Results of conceptual design studies of tilt rotor and tandem helicopter aircraft for a 200 nautical...
The results of a study of folding tilt rotor (stowed rotor) aircraft are presented. The effects of d...
A preliminary design study was conducted to establish a minimum sized, low cost V/STOL tilt-rotor re...
Conceptual design studies are summarized of tandem-rotor helicopter and tilt-rotor aircraft for a sh...
The conceptual designs of four useful tilt-rotor aircraft for the 1975 to 1980 time period are prese...
Weight standardization, tilt and stopped rotor optimization, and noise sensitivity analysis of V/STO...
A conceptual design study was conducted to define a representative military and/or commercial tilt-p...
Conceptual design studies of pure and compound helicopter commercial short-haul transport aircraft f...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
The performances of a derivative concept of a 1985 STOL tilt rotor transport, and of a second concep...
A design study was conducted for a remote lift-fan commercial V/STOL transport for the 1985 time per...
Evaluation of advanced VTOL, STOL, and conventional takeoff and landing aircraft for short haul tran...
A conceptual design study is presented of 1,985 commercial tilt rotor STOL transports for a NASA 200...
Aircraft were synthesized in the 21-, 45-, and 100- passenger categories. Technological factors were...
The STOL substantiating data are presented of a conceptual design study of 1985 commercial tilt roto...
Results of conceptual design studies of tilt rotor and tandem helicopter aircraft for a 200 nautical...
The results of a study of folding tilt rotor (stowed rotor) aircraft are presented. The effects of d...
A preliminary design study was conducted to establish a minimum sized, low cost V/STOL tilt-rotor re...
Conceptual design studies are summarized of tandem-rotor helicopter and tilt-rotor aircraft for a sh...
The conceptual designs of four useful tilt-rotor aircraft for the 1975 to 1980 time period are prese...
Weight standardization, tilt and stopped rotor optimization, and noise sensitivity analysis of V/STO...
A conceptual design study was conducted to define a representative military and/or commercial tilt-p...
Conceptual design studies of pure and compound helicopter commercial short-haul transport aircraft f...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
The performances of a derivative concept of a 1985 STOL tilt rotor transport, and of a second concep...
A design study was conducted for a remote lift-fan commercial V/STOL transport for the 1985 time per...
Evaluation of advanced VTOL, STOL, and conventional takeoff and landing aircraft for short haul tran...