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Derivation of Integrated Load Distributions from Resampled Computational DataPrincipal component analysis (PCA) has been the center of many surrogate models used to characterize fluid flows in recent years. However, little work has been done to character- ize the uncertainty in the PCA transform itself and its effect on derived surrogate models. To explore the uncertainty, a typical interpolated surrogate model is constructed for a represen- tative aerodynamic body from computational data. The computational data is then resampled to explore the robustness of the PCA transformation. The variations of the model predictions during this resampling are analyzed to get a measure of confidence in the PCA transformation, which is then applied to the interpolated surrogate model to get uncertainty on integrated force predictions. An initial test case has been explored with promising results.
Document ID
20240014371
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
T J Wignall
(Langley Research Center Hampton, United States)
Michael W Lee
(Langley Research Center Hampton, United States)
Date Acquired
November 12, 2024
Subject Category
Aerodynamics
Meeting Information
Meeting: AIAA SciTech
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: 338049.02.40.04.03.50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Principal Component Analysis
Proper Orthogonal Decomposition
Bootstrap
Computational Fluid Dynamics
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