The equations used by the 16-Foot Transonic Wind Tunnel in the data reduction programs are presented in nine modules. Each module consists of equations necessary to achieve a specific purpose. These modules are categorized in the following groups: (1) tunnel parameters; (2) jet exhaust measurements; (3) skin friction drag; (4) balance loads and model attitudes calculations; (5) internal drag (or exit-flow distribution); (6) pressure coefficients and integrated forces; (7) thrust removal options; (8) turboprop options; and (9) inlet distortion.


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    Title :

    Data Reduction Formulas for the 16-Foot Transonic Tunnel: NASA Langley Research Center, Revision 2


    Contributors:

    Publication date :

    1992


    Size :

    288 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English