Methods for quantitative prediction of behavior following initial misalignment on catapult in terms of time histories of motion; both single pendant towing arrangement and case of V-bridle considered; comparison shown between calculations and dynamically similar model typifying current jet fighter parameters.


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    Title :

    Prediction of yawing stability characteristics of airplanes during catapulting


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1952


    Size :

    11 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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