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Discrete Adjoint-Based Design for Unsteady Turbulent Flows On Dynamic Overset Unstructured GridsA discrete adjoint-based design methodology for unsteady turbulent flows on three-dimensional dynamic overset unstructured grids is formulated, implemented, and verified. The methodology supports both compressible and incompressible flows and is amenable to massively parallel computing environments. The approach provides a general framework for performing highly efficient and discretely consistent sensitivity analysis for problems involving arbitrary combinations of overset unstructured grids which may be static, undergoing rigid or deforming motions, or any combination thereof. General parent-child motions are also accommodated, and the accuracy of the implementation is established using an independent verification based on a complex-variable approach. The methodology is used to demonstrate aerodynamic optimizations of a wind turbine geometry, a biologically-inspired flapping wing, and a complex helicopter configuration subject to trimming constraints. The objective function for each problem is successfully reduced and all specified constraints are satisfied.
Document ID
20120001339
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Nielsen, Eric J.
(NASA Langley Research Center Hampton, VA, United States)
Diskin, Boris
(National Inst. of Aerospace Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
January 9, 2012
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-12832
AIAA Paper 2012-0554
Meeting Information
Meeting: 50th AIAA Aerospace Sciences Meeting and Exhibit
Location: Nashville, TN
Country: United States
Start Date: January 9, 2012
End Date: January 12, 2012
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNL09AA00A
CONTRACT_GRANT: NNL07AA23C
WBS: WBS 877868.02.07.07.03.01.02
Distribution Limits
Public
Copyright
Public Use Permitted.
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