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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Contributors:

    Publication date :

    1987


    Size :

    204 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English