An in-flight investigation was made to determine the terminal-area operating problems of a vectored-thrust-jet vertical and short take-off landing (V/STOL) airplane under simulated instrument conditions. Handling-qualities data pertinent to the terminal-area approach and landing task are presented in the text, and additional documentation is included in the appendixes. Problems dealing with the cruise letdown to localizer capture, conversion to powered-lift flight, precise control of the glide slope, approach velocity or deceleration schedule, hover, and landing are discussed.Prepared at Langley Research Center.Cover title.Bibliography: p. 21.An in-flight investigation was made to determine the terminal-area operating problems of a vectored...
A fixed-base simulator program was conducted to define the problems and methods for solution associa...
The T-33 variable stability and variable drag airplane was used in a flight program to evaluate vari...
A fixed-base simulator study was conducted to determine the minimum acceptable level of longitudinal...
A flight investigation was performed with the Dornier DO-31 VTOL to evaluate the performance, handli...
Flight characteristics of jet-flap STOL transport aircraft during approach and landin
Simulation tests were made using an experimental powered-lift STOL airplane to help define airport-a...
Transition, approach, and vertical landing tests for VTOL transport in terminal are
Longitudinal and lateral stability data were obtained with the model out of and in ground effect ove...
A fixed-base simulator study was conducted to determine the flight characteristics of a representati...
V/STOL research on controllability, display devices, pilot performance, and terminal guidanc
Simulation tests were made using an experimental powered-lift STOL airplane to help define airport-a...
A piloted simulation was performed on the Vertical Motion Simulator at NASA Ames Research Center to ...
Results are presented of a flight-test program utilizing a CV-990 airplane, flow in low-lift-to-drag...
The existing body of research to investigate airworthiness, performance, handling, and operational r...
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...
The T-33 variable stability and variable drag airplane was used in a flight program to evaluate vari...
A fixed-base simulator study was conducted to determine the minimum acceptable level of longitudinal...
A flight investigation was performed with the Dornier DO-31 VTOL to evaluate the performance, handli...
Flight characteristics of jet-flap STOL transport aircraft during approach and landin
Simulation tests were made using an experimental powered-lift STOL airplane to help define airport-a...
Transition, approach, and vertical landing tests for VTOL transport in terminal are
Longitudinal and lateral stability data were obtained with the model out of and in ground effect ove...
A fixed-base simulator study was conducted to determine the flight characteristics of a representati...
V/STOL research on controllability, display devices, pilot performance, and terminal guidanc
Simulation tests were made using an experimental powered-lift STOL airplane to help define airport-a...
A piloted simulation was performed on the Vertical Motion Simulator at NASA Ames Research Center to ...
Results are presented of a flight-test program utilizing a CV-990 airplane, flow in low-lift-to-drag...
The existing body of research to investigate airworthiness, performance, handling, and operational r...
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...
The T-33 variable stability and variable drag airplane was used in a flight program to evaluate vari...
A fixed-base simulator study was conducted to determine the minimum acceptable level of longitudinal...