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.
Computations for the 16-Foot Transonic Tunnel, NASA, Langley Research Center
1984
189 pages
Report
No indication
English
Transonic Propulsion Aerodynamics Research at NASA Langley Research Center
SAE Technical Papers | 1992
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