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A Practical Methodology for Quantifying Random and Systematic Components of Unexplained Variance in a Wind TunnelThis paper documents a check standard wind tunnel test conducted in the Langley 0.3-Meter Transonic Cryogenic Tunnel (0.3M TCT) that was designed and analyzed using the Modern Design of Experiments (MDOE). The test designed to partition the unexplained variance of typical wind tunnel data samples into two constituent components, one attributable to ordinary random error, and one attributable to systematic error induced by covariate effects. Covariate effects in wind tunnel testing are discussed, with examples. The impact of systematic (non-random) unexplained variance on the statistical independence of sequential measurements is reviewed. The corresponding correlation among experimental errors is discussed, as is the impact of such correlation on experimental results generally. The specific experiment documented herein was organized as a formal test for the presence of unexplained variance in representative samples of wind tunnel data, in order to quantify the frequency with which such systematic error was detected, and its magnitude relative to ordinary random error. Levels of systematic and random error reported here are representative of those quantified in other facilities, as cited in the references.
Document ID
20120001497
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Deloach, Richard
(NASA Langley Research Center Hampton, VA, United States)
Obara, Clifford J.
(NASA Langley Research Center Hampton, VA, United States)
Goodman, Wesley L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
January 9, 2012
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-14030
AIAA Paper 2012-0764
Report Number: NF1676L-14030
Report Number: AIAA Paper 2012-0764
Meeting Information
Meeting: 50th AIAA Aerospace Sciences Meeting and Exhibit
Location: Nashville, TN
Country: United States
Start Date: January 9, 2012
End Date: January 12, 2012
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 122711.03.09.07.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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