Add to ORKGResults of conceptual design studies of tilt rotor and tandem helicopter aircraft for a 200 nautical mile commercial short haul transport mission are presented. The trade study data used in selecting the design point aircraft and technology details necessary to support the design conclusions are included
Weight standardization, tilt and stopped rotor optimization, and noise sensitivity analysis of V/STO...
Results of conceptual design studies of commercial rotary wing transport aircraft for the 1985 time ...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
Results of conceptual engineering design studies of a STOL tilt rotor commercial aircraft for the 19...
Aircraft were synthesized in the 21-, 45-, and 100- passenger categories. Technological factors were...
Conceptual design studies are summarized of tandem-rotor helicopter and tilt-rotor aircraft for a sh...
A conceptual design study is presented of 1,985 commercial tilt rotor STOL transports for a NASA 200...
Conceptual design studies of pure and compound helicopter commercial short-haul transport aircraft f...
A preliminary design study was conducted to establish a minimum sized, low cost V/STOL tilt-rotor re...
The STOL substantiating data are presented of a conceptual design study of 1985 commercial tilt roto...
Evaluation of advanced VTOL, STOL, and conventional takeoff and landing aircraft for short haul tran...
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...
In anticipation of an eventual VTOL requirement for civil aviation, NASA has been conducting studies...
Weight standardization, tilt and stopped rotor optimization, and noise sensitivity analysis of V/STO...
Results of conceptual design studies of commercial rotary wing transport aircraft for the 1985 time ...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
Results of conceptual engineering design studies of a STOL tilt rotor commercial aircraft for the 19...
Aircraft were synthesized in the 21-, 45-, and 100- passenger categories. Technological factors were...
Conceptual design studies are summarized of tandem-rotor helicopter and tilt-rotor aircraft for a sh...
A conceptual design study is presented of 1,985 commercial tilt rotor STOL transports for a NASA 200...
Conceptual design studies of pure and compound helicopter commercial short-haul transport aircraft f...
A preliminary design study was conducted to establish a minimum sized, low cost V/STOL tilt-rotor re...
The STOL substantiating data are presented of a conceptual design study of 1985 commercial tilt roto...
Evaluation of advanced VTOL, STOL, and conventional takeoff and landing aircraft for short haul tran...
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...
In anticipation of an eventual VTOL requirement for civil aviation, NASA has been conducting studies...
Weight standardization, tilt and stopped rotor optimization, and noise sensitivity analysis of V/STO...
Results of conceptual design studies of commercial rotary wing transport aircraft for the 1985 time ...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...