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The pros and cons of code validationComputational and wind tunnel error sources are examined and quantified using specific calculations of 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
19890000663
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bobbitt, Percy J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-100657
NAS 1.15:100657
AIAA PAPER 88-2535
Meeting Information
Meeting: AIAA Applied Aerodynamic Conference
Location: Williamsburg, VA
Country: United States
Start Date: June 6, 1988
End Date: June 8, 1988
Accession Number
89N10034
Funding Number(s)
PROJECT: RTOP 505-61-01-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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