Add to ORKGThe results of a real time piloted simulation to investigate the handling qualities and performance of a tilting rotor aircraft design are presented. The aerodynamic configuration of the aircraft is described. The procedures for conducting the simulator evaluation are reported. Pilot comments of the aircraft handling qualities under various simulated flight conditions are included. The time histories of selected pilot maneuvers are shown
The design characteristics of the XV-15 Tilt rotor research aircraft are presented. Particular atten...
The results of a study of the use of composite materials in the wing of a tilt rotor aircraft are pr...
An experimental research program has been conducted on a series of tilt rotors designed for a range ...
A mathematical model for a real time simulation of a tilt rotor aircraft was developed. The mathemat...
A mathematical model for real-time flight simulation of a tilt rotor research aircraft was developed...
A preliminary design study was conducted to establish a minimum sized, low cost V/STOL tilt-rotor re...
The design features and general characteristics of the NASA/Army XV-15 tilt rotor research aircraft ...
The results of a study of folding tilt rotor (stowed rotor) aircraft are presented. The effects of d...
A mathematical model of a tilt-wing aircraft that was used in a piloted, six-degree-of-freedom fligh...
The response to vertical turbulence in cruise of the HTR XV-15 design is studied using simulation te...
A piloted simulation of an advanced hingeless rotor XV-15 tilt-rotor aircraft was carried out. The e...
The conceptual designs of four useful tilt-rotor aircraft for the 1975 to 1980 time period are prese...
Several ground-based simulation experiments undertaken to investigate concerns related to tilt-rotor...
A two-phase piloted simulation study was conducted to investigate alternative wing and flap controls...
A two phase piloted simulation study has been conducted in the Ames Vertical Motion Simulator to inv...
The design characteristics of the XV-15 Tilt rotor research aircraft are presented. Particular atten...
The results of a study of the use of composite materials in the wing of a tilt rotor aircraft are pr...
An experimental research program has been conducted on a series of tilt rotors designed for a range ...
A mathematical model for a real time simulation of a tilt rotor aircraft was developed. The mathemat...
A mathematical model for real-time flight simulation of a tilt rotor research aircraft was developed...
A preliminary design study was conducted to establish a minimum sized, low cost V/STOL tilt-rotor re...
The design features and general characteristics of the NASA/Army XV-15 tilt rotor research aircraft ...
The results of a study of folding tilt rotor (stowed rotor) aircraft are presented. The effects of d...
A mathematical model of a tilt-wing aircraft that was used in a piloted, six-degree-of-freedom fligh...
The response to vertical turbulence in cruise of the HTR XV-15 design is studied using simulation te...
A piloted simulation of an advanced hingeless rotor XV-15 tilt-rotor aircraft was carried out. The e...
The conceptual designs of four useful tilt-rotor aircraft for the 1975 to 1980 time period are prese...
Several ground-based simulation experiments undertaken to investigate concerns related to tilt-rotor...
A two-phase piloted simulation study was conducted to investigate alternative wing and flap controls...
A two phase piloted simulation study has been conducted in the Ames Vertical Motion Simulator to inv...
The design characteristics of the XV-15 Tilt rotor research aircraft are presented. Particular atten...
The results of a study of the use of composite materials in the wing of a tilt rotor aircraft are pr...
An experimental research program has been conducted on a series of tilt rotors designed for a range ...