Data reduction formulas for the 16-foot transonic tunnel: NASA Langley Research Center, revision 2

Data reduction formulas for the 16-foot transonic tunnel: NASA Langley Research Center, revision 2

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;...

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Bibliographische Detailangaben
Hauptverfasser: Mercer, Charles E., Berrier, Bobby L., Capone, Francis J., Grayston, Alan M.
Format: Report
Sprache:eng
Schlagworte:
Research And Support Facilities (Air)
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Zusammenfassung: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.