For abstract, see N76-16033.


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    Title :

    Aerodynamic Results of a Separation Test (CA20) Conducted at the Boeing Transonic Wind Tunnel Using 0.030-Scale Models of the Configuration 140A/B (Modified) Ssv Orbiter (Model No. 45-0) and the Boeing 747 Carrier (Model No. Ax 1319 I-1), Volume 3


    Contributors:
    T. Dziubala (author) / V. Esparza (author) / R. L. Gillins (author) / M. Petrozzi (author)

    Publication date :

    1975


    Size :

    1106 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English