Stability and control problems which result from inertia coupling during roll maneuvers is of particular concern in design of fighter and interceptor aircraft, where high rolling rate and large amplitude roll maneuvers are critically required; important aircraft design implications resulting from consideration of this type of maneuver.


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    Title :

    Airplane design implications of inertia coupling problem


    Additional title:

    Aeronautical Eng Rev


    Contributors:
    Heppe, R.R. (author) / Celniker, L. (author)

    Published in:

    Publication date :

    1957


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Intercooling problem in airplane design

    Dickinson, H.B. | Engineering Index Backfile | 1944


    Intercooling problem in airplane design

    Dickinson, H.B. | Engineering Index Backfile | 1944