Add to ORKGA project to develop an experimental aircraft for use as an inflight demonstrator of the augmentor wing, short takeoff concept is discussed. The required modifications were made on a de Havilland C-8A aircraft. The modifications to the aircraft are explained and the performance of the modified aircraft is reported
Flight characteristics of jet-flap STOL transport aircraft during approach and landin
Test results are presented for a large scale, external augmentor V/STOL model in a 40 ft by 80 ft wi...
Several different flight research programs carried out by NASA and the Canadian Government using the...
An existing deHavilland C-8A airplane has been modified into an augmentor wing flight test vehicle. ...
Design study data for CV-7A transport aircraft modification to provide augmentor wing jet STOL resea...
The flight test program objectives are: (1) To determine the in-flight aerodynamic, performance, and...
Exploratory design studies conducted to establish the configuration of an augmentor wing vruise blow...
Modifications were made to the model to improve longitudinal acceleration capability during transiti...
This program was undertaken to develop, through analysis, design, experimental static testing, wind ...
Static performance and acoustic tests were conducted on a two-dimensional one-third-scale augmentor ...
The experience gained in over four years of STOL operations with the augmentor wing research aircraf...
A simulator study of STOL airworthiness was conducted using a model of an augmentor wing transport. ...
Aerodynamic design data for the Augmented Jet Flap STOL Research Aircraft or commonly known as the A...
Analytical design and wind tunnel test evaluations covering the feasibility of applying wing tip ext...
A preliminary design study was conducted to establish a minimum sized, low cost V/STOL tilt-rotor re...
Flight characteristics of jet-flap STOL transport aircraft during approach and landin
Test results are presented for a large scale, external augmentor V/STOL model in a 40 ft by 80 ft wi...
Several different flight research programs carried out by NASA and the Canadian Government using the...
An existing deHavilland C-8A airplane has been modified into an augmentor wing flight test vehicle. ...
Design study data for CV-7A transport aircraft modification to provide augmentor wing jet STOL resea...
The flight test program objectives are: (1) To determine the in-flight aerodynamic, performance, and...
Exploratory design studies conducted to establish the configuration of an augmentor wing vruise blow...
Modifications were made to the model to improve longitudinal acceleration capability during transiti...
This program was undertaken to develop, through analysis, design, experimental static testing, wind ...
Static performance and acoustic tests were conducted on a two-dimensional one-third-scale augmentor ...
The experience gained in over four years of STOL operations with the augmentor wing research aircraf...
A simulator study of STOL airworthiness was conducted using a model of an augmentor wing transport. ...
Aerodynamic design data for the Augmented Jet Flap STOL Research Aircraft or commonly known as the A...
Analytical design and wind tunnel test evaluations covering the feasibility of applying wing tip ext...
A preliminary design study was conducted to establish a minimum sized, low cost V/STOL tilt-rotor re...
Flight characteristics of jet-flap STOL transport aircraft during approach and landin
Test results are presented for a large scale, external augmentor V/STOL model in a 40 ft by 80 ft wi...
Several different flight research programs carried out by NASA and the Canadian Government using the...