Several important configuration features are discussed relative to adaptation of Lockheed XH-51A rigid rotor to compound research flight vehicle; testing undertaken to support XH-51A compound program included flight test of both three and four-bladed rotor helicopter; flight tests of compound research vehicle through Phase I and Phase II and results in terms of measured data and handling characteristics are presented; flight tests peculiar to compound aircraft are discussed along with pilot qualitative comments.


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    Title :

    XH-51a compound research flight test program


    Additional title:

    Can Aeronatuics Space J


    Contributors:


    Publication date :

    1967


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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