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)


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    Title :

    A Flight Investigation of the STOL Characteristics of an Augmented Jet Flap STOL Research Aircraft


    Contributors:
    H. C. Quigley (author) / R. C. Innis (author) / S. Grossmith (author)

    Publication date :

    1974


    Size :

    143 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English