The equations used by the 16 foot transonic tunnel in the data reduction programs are presented in eight modules. Each module consists of equations necessary to achieve a specific purpose. These modules are categorized in the following groups: tunnel parameters; jet exhaust measurements; skin friction drag; balance loads and model attitudes calculations; internal drag (or exit-flow distributions); pressure coefficients and integrated forces; thrust removal options; and turboprop options. This document is a companion document to NASA TM-83186, A User's Guide to the Langley 16 Foot Transonic Tunnel, August 1981.


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    Titel :

    Computations for the 16-Foot Transonic Tunnel, NASA (National Aeronautics and Space Administration) Langley Research Center, Revision 1


    Beteiligte:
    C. E. Mercer (Autor:in) / B. L. Berrier (Autor:in) / F. J. Capone (Autor:in) / A. M. Grayston (Autor:in) / C. D. Sherman (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    204 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch