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Techniques in Assessing Random Uncertainty of Wind Tunnel Replicate Test DataThe preferred method to determine the random uncertainty of variables of interest during wind tunnel tests is by direct analysis of replicate data. However, current information is limited to analysis of a single replicate set condition that does not consider data covariance. This paper provides additional information on considerations for quantifying random uncertainty including the evaluation and correction of replicate data covariance, the selection of replicate set conditions for the test, and the interpolation of random uncertainty at other than replicate set conditions. The analysis and techniques are supported by data from a conventional aircraft configuration test at the Oran Nicks Low-Speed Wind Tunnel and an ASME nozzle flow characterization at the Propulsion Systems Laboratory.
Document ID
20240015411
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Drew A Curriston
(United States Military Academy West Point, New York, United States)
Edward B White
(The University of Texas at Dallas Richardson, United States)
Erin P Hubbard
(Glenn Research Center Cleveland, United States)
Date Acquired
December 2, 2024
Subject Category
Aircraft Design, Testing and Performance
Quality Assurance and Reliability
Meeting Information
Meeting: AIAA SciTech Forum
Location: Orlando, FL
Country: US
Start Date: January 6, 2025
End Date: January 10, 2025
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 951888.04.03.10
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Keywords
Uncertainty
Random Uncertainty
Replicate Data
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