An analytical and experimental investigation has been made to provide a space shuttle orbiter wing design that met the guideline requirements of landing performance, stability, and hypersonic trim for a specified center-of-gravity envelope. The analytical study was facilitated by the use of the Optimal Design Integration system (ODIN) and the experimental part of the investigation was conducted in the Langley low-turbulence pressure tunnel and the Langley continuous-flow hypersonic tunnel. (Author)


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    Titel :

    Computer-Aided Space Shuttle Orbiter Wing Design Study


    Beteiligte:
    W. P. Phillips (Autor:in) / J. P. Decker (Autor:in) / T. R. Rau (Autor:in) / C. R. Glatt (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    84 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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