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)


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    Title :

    The Development of an Augmentor Wing Jet STOL Research Airplane (Modified C-8A). Volume 1: Summary


    Contributors:
    R. H. Ashleman (author) / H. Kavdahl (author)

    Publication date :

    1972


    Size :

    182 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English