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: (1) wind tunnel parameters, (2) jet exhaust measurements, (3) skin friction drag, (4) balance loads and model attitudes, (5) internal drag (or exit flow distributions), (6) pressure coefficients and integrated forces, (7) thrust removal options, and (8) turboprop options.


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    Title :

    Computations for the 16-Foot Transonic Tunnel, NASA, Langley Research Center


    Contributors:

    Publication date :

    1984


    Size :

    189 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English