The requirements for a new research aircraft to provide in-flight V/STOL simulation were reviewed. The required capabilities were based on known limitations of ground based simulation and past/current experience with V/STOL inflight simulation. Results indicate that V/STOL inflight simulation capability is needed to aid in the design and development of high performance V/STOL aircraft. Although a new research V/STOL aircraft is preferred, an interim solution can be provided by use of the X-22A, the CH-47B, or the 4AV-8B aircraft modified for control/display flight research
Several ground-based simulation experiments undertaken to investigate concerns related to tilt-rotor...
The United States is in the initial stages of committing to a national program to develop a superson...
A flight simulation program was conducted on the flight simulator for advanced aircraft (FSAA). The ...
The requirements for satisfactory characteristics in several key technology areas are discussed and ...
Results of a substantial body of ground-based simulation experiments indicate that a high degree of ...
Nonhelicopter types of V/STOL aircraft developed in the United States are reviewed, and some lessons...
Simulations of V/STOL aircraft for autopilot research were introduced as examples of large scale sys...
The impact of military applications on rotorcraft and V/STOL aircraft design is summarized with resp...
This paper describes three government-conducted, piloted flight simulations of the Grumman Design 69...
The status of the major NASA/Army capabilities in piloted rotorcraft flight simulation is reviewed. ...
A study has been undertaken to define hand-ling qualities criteria for V/STOL aircraft. With the cur...
A fixed-base simulator study was conducted to determine the minimum acceptable level of longitudinal...
A simulator study of short takeoff and landing (STOL) aircraft was conducted using a model of a defl...
The aerodynamic performance of V/STOL and STOVL fighter/attack aircraft was assessed. Aerodynamic an...
The operating problems and equipment requirements for STOL airplanes in terminal area operations in ...
Several ground-based simulation experiments undertaken to investigate concerns related to tilt-rotor...
The United States is in the initial stages of committing to a national program to develop a superson...
A flight simulation program was conducted on the flight simulator for advanced aircraft (FSAA). The ...
The requirements for satisfactory characteristics in several key technology areas are discussed and ...
Results of a substantial body of ground-based simulation experiments indicate that a high degree of ...
Nonhelicopter types of V/STOL aircraft developed in the United States are reviewed, and some lessons...
Simulations of V/STOL aircraft for autopilot research were introduced as examples of large scale sys...
The impact of military applications on rotorcraft and V/STOL aircraft design is summarized with resp...
This paper describes three government-conducted, piloted flight simulations of the Grumman Design 69...
The status of the major NASA/Army capabilities in piloted rotorcraft flight simulation is reviewed. ...
A study has been undertaken to define hand-ling qualities criteria for V/STOL aircraft. With the cur...
A fixed-base simulator study was conducted to determine the minimum acceptable level of longitudinal...
A simulator study of short takeoff and landing (STOL) aircraft was conducted using a model of a defl...
The aerodynamic performance of V/STOL and STOVL fighter/attack aircraft was assessed. Aerodynamic an...
The operating problems and equipment requirements for STOL airplanes in terminal area operations in ...
Several ground-based simulation experiments undertaken to investigate concerns related to tilt-rotor...
The United States is in the initial stages of committing to a national program to develop a superson...
A flight simulation program was conducted on the flight simulator for advanced aircraft (FSAA). The ...