Add to ORKGThe conceptual designs of four useful tilt-rotor aircraft for the 1975 to 1980 time period are presented. Parametric studies leading to design point selection are described, and the characteristics and capabilities of each configuration are presented. An assessment is made of current technology status, and additional tilt-rotor research programs are recommended to minimize the time, cost, and risk of development of these vehicles
A mathematical model for real-time flight simulation of a tilt rotor research aircraft was developed...
A mathematical model for a real time simulation of a tilt rotor aircraft was developed. The mathemat...
The STOL substantiating data are presented of a conceptual design study of 1985 commercial tilt roto...
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...
A conceptual design study is presented of 1,985 commercial tilt rotor STOL transports for a NASA 200...
The design features and general characteristics of the NASA/Army XV-15 tilt rotor research aircraft ...
Results of conceptual engineering design studies of a STOL tilt rotor commercial aircraft for the 19...
The results of a study of the use of composite materials in the wing of a tilt rotor aircraft are pr...
A conceptual design study was conducted to define a representative military and/or commercial tilt-p...
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...
The results of a real time piloted simulation to investigate the handling qualities and performance ...
Tilt-rotor technology has many features which make it a very promising development in aviation which...
Results of conceptual design studies of tilt rotor and tandem helicopter aircraft for a 200 nautical...
A mathematical model for real-time flight simulation of a tilt rotor research aircraft was developed...
A mathematical model for a real time simulation of a tilt rotor aircraft was developed. The mathemat...
The STOL substantiating data are presented of a conceptual design study of 1985 commercial tilt roto...
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...
A conceptual design study is presented of 1,985 commercial tilt rotor STOL transports for a NASA 200...
The design features and general characteristics of the NASA/Army XV-15 tilt rotor research aircraft ...
Results of conceptual engineering design studies of a STOL tilt rotor commercial aircraft for the 19...
The results of a study of the use of composite materials in the wing of a tilt rotor aircraft are pr...
A conceptual design study was conducted to define a representative military and/or commercial tilt-p...
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...
The results of a real time piloted simulation to investigate the handling qualities and performance ...
Tilt-rotor technology has many features which make it a very promising development in aviation which...
Results of conceptual design studies of tilt rotor and tandem helicopter aircraft for a 200 nautical...
A mathematical model for real-time flight simulation of a tilt rotor research aircraft was developed...
A mathematical model for a real time simulation of a tilt rotor aircraft was developed. The mathemat...
The STOL substantiating data are presented of a conceptual design study of 1985 commercial tilt roto...