Recent developments in study of effects of structural flexibility on stability and control; literature reviewed against theoretical background assessing importance of these effects and establishing how elaborate mathematical treatment is necessary to predict them with reasonable accuracy; advantages of integrated approach.


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    Title :

    Present status of aircraft stability problems in aeroelastic domain


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1959


    Size :

    12 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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