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    Wind Tunnel Tests for Separation Dynamics Modeling of a Two-Stage Hypersonic Vehicle

    Wind Tunnel Tests for Separation Dynamics Modeling of a Two-Stage Hypersonic Vehicle


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    Title :

    Wind Tunnel Tests for Separation Dynamics Modeling of a Two-Stage Hypersonic Vehicle

    Contributors:
    Breitsamter, C. (author) / Laschka, B. (author) / ZShringer, C. (author) / Sachs, G. (author) / American Institute of Aeronautics and Astronautics
    Conference:

    International conference; 10th, Space planes and hypersonic systems and technologies ; 2001 ; Kyoto, Japan

    Published in:

    Space planes and hypersonic systems and technologies ; 308-317

    INTERNATIONAL SPACE PLANES AND HYPERSONIC SYSTEMS AND TECHNOLOGIES CONFERENCE ; 1

    Publication date :

    2001-01-01

    Size :

    10 pages

    Remarks:

    Contains papers AIAA-2001-1750 to 1927 only with gaps

    ISBN :

    1563474786

    Type of media :

    Conference paper

    Type of material :

    Print

    Language :

    English

    Keywords :

    space planes , hypersonic systems , AIAA , aeronautics , astronautics , hypersonic technologies

    © Metadata Copyright the British Library Board and other contributors. All rights reserved.

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