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Approach for Uncertainty Propagation and Robust Design in CFD Using Sensitivity DerivativesThis paper presents an implementation of the approximate statistical moment method for uncertainty propagation and robust optimization for a quasi 1-D Euler CFD (computational fluid dynamics) code. Given uncertainties in statistically independent, random, normally distributed input variables, a first- and second-order statistical moment matching procedure is performed to approximate the uncertainty in the CFD output. Efficient calculation of both first- and second-order sensitivity derivatives is required. In order to assess the validity of the approximations, the moments are compared with statistical moments generated through Monte Carlo simulations. The uncertainties in the CFD input variables are also incorporated into a robust optimization procedure. For this optimization, statistical moments involving first-order sensitivity derivatives appear in the objective function and system constraints. Second-order sensitivity derivatives are used in a gradient-based search to successfully execute a robust optimization. The approximate methods used throughout the analyses are found to be valid when considering robustness about input parameter mean values.
Document ID
20010039415
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Putko, Michele M.
(Old Dominion Univ. Norfolk, VA United States)
Newman, Perry A.
(NASA Langley Research Center Hampton, VA United States)
Taylor, Arthur C., III
(Old Dominion Univ. Norfolk, VA United States)
Green, Lawrence L.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2001-2528
Report Number: AIAA Paper 2001-2528
Meeting Information
Meeting: AIAA 15th Computational Fluid Dynamics Conference
Location: Anaheim, CA
Country: United States
Start Date: June 11, 2001
End Date: June 14, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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