Design requirements of Bell X-22A, designed to explore mechanical and aerodynamic characteristics of dual-tandem, ducted-propeller V/STOL concept and to assess its military potential; description and general arrangement of aircraft, performance and control; variable stability and control system; handling characteristics in hover and transition; stall investigations and leading data.


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    Title :

    Bell X-22A


    Additional title:

    Flight


    Contributors:

    Published in:

    Publication date :

    1967


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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