A 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.
The development of an augmentor wing jet STOL research airplane (modified C-8A). Volume 1: Summary
1972-08-01
Report
No indication
English