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. (Author)
The Development of an Augmentor Wing Jet STOL Research Airplane (Modified C-8A). Volume 1: Summary
1972
182 pages
Report
No indication
English