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Adaptive Shape Control for Aerodynamic DesignWe present an approach to aerodynamic optimization in which the shape control is adaptively parameterized. Starting from a coarse set of design variables, a sequence of higher-dimensional nested search spaces is automatically generated. Refinement can be either uniform or adaptive, in which case only the most important shape control is added. The relative importance of candidate design variables is determined by comparing objective and constraint gradients, computed at low cost via adjoint solutions. A search procedure for finding an effective ensemble of shape parameters is also given. We first demonstrate this system on a multipoint drag miminization problem in 2D with many constraints, showing that an adaptive parameterization approach consistently achieves smoother, more robust, and faster design improvement than fixed parameterizations. We also establish a 3D shape- matching benchmark, where we demonstrate that our approach automatically discovers the necessary parameters to match a target shape. By largely automating shape parameterization, this work also aims to remove a time-consuming aspect of shape optimization.
Document ID
20190001786
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Anderson, George R.
(Stanford Univ. Stanford, CA, United States)
Aftosmis, Michael J.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
March 22, 2019
Publication Date
January 5, 2015
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN19730
Report Number: ARC-E-DAA-TN19730
Meeting Information
Meeting: AIAA Aerospace Sciences Meeting
Location: Kissimmee, FL
Country: United States
Start Date: January 5, 2015
End Date: January 9, 2015
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
CONTRACT_GRANT: NNX14AF94A
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Aerodynamic Design
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