The report is Volume 2 of a three volume series. Tables of aerodynamic test data are given, including balance cavity and base pressure coefficients, axial force for aerodynamic and thrust phases, canard position, and force and moment coefficients for a series of runs.


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    Title :

    Transonic Wind Tunnel Tests on a Missile Model with Canard Wings. Volume II


    Contributors:

    Publication date :

    1973


    Size :

    674 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English