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The pros and cons of code validationComputational and wind tunnel error sources are examined and quantified using specific calculations or experimental data, and a substantial comparison of theoretical and experimental results, or a code validation, is discussed. Wind tunnel error sources considered include wall interference, sting effects, Reynolds number effects, flow quality and transition, and instrumentation such as strain gage balances, electronically scanned pressure systems, hot film gages, hot wire anemometers, and laser velocimeters. Computational error sources include math model equation sets, the solution algorithm, artificial viscosity/dissipation, boundary conditions, the uniqueness of solutions, grid resolution, turbulence modeling, and Reynolds number effects. It is concluded that although improvements in theory are being made more quickly than in experiments, wind tunnel research has the advantage of the more realistic transition process of a right turbulence model in a free-transition test.
Document ID
19880054898
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bobbitt, Percy J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1988
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 88-2535
Accession Number
88A42125
Distribution Limits
Public
Copyright
Other

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