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

    Publication date :

    1975-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :