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A Surrogate Approach to the Experimental Optimization of Multielement AirfoilsThe incorporation of experimental test data into the optimization process is accomplished through the use of Bayesian-validated surrogates. In the surrogate approach, a surrogate for the experiment (e.g., a response surface) serves in the optimization process. The validation step of the framework provides a qualitative assessment of the surrogate quality, and bounds the surrogate-for-experiment error on designs "near" surrogate-predicted optimal designs. The utility of the framework is demonstrated through its application to the experimental selection of the trailing edge ap position to achieve a design lift coefficient for a three-element airfoil.
Document ID
20040110894
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Otto, John C.
(NASA Langley Research Center Hampton, VA, United States)
Landman, Drew
(Old Dominion Univ. Norfolk, VA, United States)
Patera, Anthony T.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 7, 2013
Publication Date
July 12, 1996
Subject Category
Systems Analysis And Operations Research
Report/Patent Number
AIAA Paper 96-4138
Report Number: AIAA Paper 96-4138
Meeting Information
Meeting: Sixth AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
Location: Belevue, WA
Country: United States
Start Date: September 4, 1996
End Date: September 6, 1996
Sponsors: Department of the Air Force, American Inst. of Aeronautics and Astronautics, International Society of Structural and Multidisciplinary Optimization, NASA Headquarters
Funding Number(s)
CONTRACT_GRANT: F49620-94-1-0121
CONTRACT_GRANT: NAS1-19858
CONTRACT_GRANT: N00014-91-J-1889
CONTRACT_GRANT: NAG1-1750
CONTRACT_GRANT: NAG1-1613
Distribution Limits
Public
Copyright
Public Use Permitted.
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