Flight tests were conducted of a twin engine airplane modified to a STOL configuration with rotating cylinder flaps and interconnected propellers. The flight tests included verification of the functional operation of the rotating cylinder flap system and the determination of the low speed flying qualities and performance characteristics with emphasis on approach and landing.


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    Title :

    Flight tests of a rotating cylinder flap on a North American Rockwell YOV-10 aircraft


    Contributors:

    Publication date :

    1972-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :