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Adjoint-Based Algorithms for Adaptation and Design Optimizations on Unstructured GridsSchemes based on discrete adjoint algorithms present several exciting opportunities for significantly advancing the current state of the art in computational fluid dynamics. Such methods provide an extremely efficient means for obtaining discretely consistent sensitivity information for hundreds of design variables, opening the door to rigorous, automated design optimization of complex aerospace configuration using the Navier-Stokes equation. Moreover, the discrete adjoint formulation provides a mathematically rigorous foundation for mesh adaptation and systematic reduction of spatial discretization error. Error estimates are also an inherent by-product of an adjoint-based approach, valuable information that is virtually non-existent in today's large-scale CFD simulations. An overview of the adjoint-based algorithm work at NASA Langley Research Center is presented, with examples demonstrating the potential impact on complex computational problems related to design optimization as well as mesh adaptation.
Document ID
20060002217
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Nielsen, Eric J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2006
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: East West High Speed Flow Field Conference 2005 (EWHSFF 2005)
Location: Beijing
Country: China
Start Date: October 19, 2005
End Date: October 22, 2005
Funding Number(s)
OTHER: 23-065-30-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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