The flight test program objectives are: (1) To determine the in-flight aerodynamic, performance, and handling qualities of a jet STOL aircraft incor- porating the augmented jet flap concept; (2) to compare the results obtained in flight with characteristics predicted from wind tunnel and simulator test results; (3) to contribute to the development of criteria for design and operation of jet STOL transport aircraft; and (4) to provide a jet STOL transport aircraft for STOL systems research and development. Results obtained during the first 8 months of proof-of-concept flight testing of the aircraft in STOL configurations are reported. Included are a brief description of the aircraft, fan-jet engines, and systems; a discussion of the aerodynamic, stability and control, and STOL performance; and pilot opinion of the handling qualities and operational characteristics. (Author)
A Flight Investigation of the STOL Characteristics of an Augmented Jet Flap STOL Research Aircraft
1974
143 pages
Report
No indication
English
Flight directors for STOl aircraft
NTRS | 1983
|A Flight Investigation of a STOL Aircraft
NTIS | 1971
|