Computations for the 16-foot transonic tunnel, NASA, Langley Research Center, revision 1

Computations for the 16-foot transonic tunnel, NASA, Langley Research Center, revision 1

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 fricti...

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