Wind tunnel tests on aspect ratio 2.17 delta wing model with midchord boundary layer control flaps


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    Title :

    Large-scale wind-tunnel tests on an aspect ratio 2.17 delta-wing model equipped with midchord boundary-layer-control flaps


    Contributors:

    Publication date :

    1964-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English