Four different methods for determination of sideslip angle, vertical tail angle of attack, and vertical tail load during rolling pullout maneuver; airplane configurations considered are straight wing, swept wing, and delta wing type.


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    Title :

    Analysis of rolling pull-out maneuver


    Additional title:

    J Aeronautical Sciences


    Contributors:

    Published in:

    Publication date :

    1956


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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