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Prediction Interval Development for Wind-Tunnel Balance Check-LoadingResults from the Facility Analysis Verification and Operational Reliability project revealed a critical gap in capability in ground-based aeronautics research applications. Without a standardized process for check-loading the wind-tunnel balance or the model system, the quality of the aerodynamic force data collected varied significantly between facilities. A prediction interval is required in order to confirm a check-loading. The prediction interval provides an expected upper and lower bound on balance load prediction at a given confidence level. A method has been developed which accounts for sources of variability due to calibration and check-load application. The prediction interval method of calculation and a case study demonstrating its use is provided. Validation of the methods is demonstrated for the case study based on the probability of capture of confirmation points.
Document ID
20140006540
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Landman, Drew
(Old Dominion Univ. Norfolk, VA, United States)
Toro, Kenneth G.
(Old Dominion Univ. Norfolk, VA, United States)
Commo, Sean A.
(NASA Langley Research Center Hampton, VA, United States)
Lynn, Keith C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
June 3, 2014
Publication Date
May 19, 2014
Subject Category
Instrumentation And Photography
Report/Patent Number
NF1676L-18378
Report Number: NF1676L-18378
Meeting Information
Meeting: International Symposium on Strain-Gauge Balances
Location: Seattle, WA
Country: United States
Start Date: May 19, 2014
End Date: May 22, 2014
Funding Number(s)
WBS: WBS 122711.03.09.07.02
Distribution Limits
Public
Copyright
Public Use Permitted.
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