Add to ORKGA fixed-base simulator study was conducted to determine the flight characteristics of a representative STOL transport having a high wing and equipped with an external-flow jet flap in combination with four high-bypass-ratio fan-jet engines during the approach and landing. Real-time digital simulation techniques were used. The computer was programed with equations of motion for six degrees of freedom and the aerodynamic inputs were based on measured wind-tunnel data. A visual display of a STOL airport was provided for simulation of the flare and touchdown characteristics. The primary piloting task was an instrument approach to a breakout at a 200-ft ceiling with a visual landing
The operating problems and equipment requirements for STOL airplanes in terminal area operations in ...
Simulator study of instrument landing approach of heavy subsonic jet transport with external-flow je...
Takeoff and landing performance characteristics and field length requirements were determined analyt...
Flight characteristics of jet-flap STOL transport aircraft during approach and landin
A piloted simulation study has been made of typical landing approaches with an externally blown flap...
A fixed-base simulator program was conducted to define the problems and methods for solution associa...
A moving-base simulator investigation of the problems of recovery and landing of a STOL aircraft aft...
A fixed-base simulator study was conducted to determine the minimum acceptable level of longitudinal...
The simulation employed all six rigid-body degrees of freedom and incorporated aerodynamic character...
A fixed-base visual simulation study has been conducted to evaluate the use of decoupled controls as...
The low-speed flying qualities of an experimental STOL configuration were evaluated by using a fixed...
An analysis of the influence of engine response characteristics on the approach and landing of an ex...
A simulator study of short takeoff and landing (STOL) aircraft was conducted using a model of a defl...
Investigation of the influence of engine response characteristics on approach and landing operations...
Simulation tests were made using an experimental powered-lift STOL airplane to help define airport-a...
The operating problems and equipment requirements for STOL airplanes in terminal area operations in ...
Simulator study of instrument landing approach of heavy subsonic jet transport with external-flow je...
Takeoff and landing performance characteristics and field length requirements were determined analyt...
Flight characteristics of jet-flap STOL transport aircraft during approach and landin
A piloted simulation study has been made of typical landing approaches with an externally blown flap...
A fixed-base simulator program was conducted to define the problems and methods for solution associa...
A moving-base simulator investigation of the problems of recovery and landing of a STOL aircraft aft...
A fixed-base simulator study was conducted to determine the minimum acceptable level of longitudinal...
The simulation employed all six rigid-body degrees of freedom and incorporated aerodynamic character...
A fixed-base visual simulation study has been conducted to evaluate the use of decoupled controls as...
The low-speed flying qualities of an experimental STOL configuration were evaluated by using a fixed...
An analysis of the influence of engine response characteristics on the approach and landing of an ex...
A simulator study of short takeoff and landing (STOL) aircraft was conducted using a model of a defl...
Investigation of the influence of engine response characteristics on approach and landing operations...
Simulation tests were made using an experimental powered-lift STOL airplane to help define airport-a...
The operating problems and equipment requirements for STOL airplanes in terminal area operations in ...
Simulator study of instrument landing approach of heavy subsonic jet transport with external-flow je...
Takeoff and landing performance characteristics and field length requirements were determined analyt...