Report discusses numerical simulations of flow of air about integrated Space Shuttle in ascent. Goal: to improve understanding of, and ability to predict, how integrated Space Shuttle will perform during both nominal and aborted ascent under various conditions. These and other numerical simulations intended both to supplement wind-tunnel data, corrupted to some extent by scaling and wall-interference effects, and to compensate for scarcity of valid flight data.


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    Title :

    Computed Flow About The Integrated Space Shuttle


    Contributors:
    Buning, P. G. (author) / Chiu, I. T. (author) / Obayashi, S. (author) / Rizk, Y. M. (author) / Steger, J. L. (author)

    Published in:

    Publication date :

    1991-10-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :



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