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Adjoint Method for Aerodynamic Shape Improvement in Comparison with Surface Pressure Gradient Method

Journal Article
2011-01-0151
ISSN: 1946-3995, e-ISSN: 1946-4002
Published April 12, 2011 by SAE International in United States
Adjoint Method for Aerodynamic Shape Improvement in Comparison with Surface Pressure Gradient Method
Sector:
Citation: Han, T., Hill, C., and Jindal, S., "Adjoint Method for Aerodynamic Shape Improvement in Comparison with Surface Pressure Gradient Method," SAE Int. J. Passeng. Cars – Mech. Syst. 4(1):100-107, 2011, https://doi.org/10.4271/2011-01-0151.
Language: English

References

  1. Han, T. Kim, Y. “Aerodynamic Shape Improvement Based on Surface Pressure Gradients in the Stream-wise and the Transverse Directions,” SAE Technical Paper 2010-01-0511 2010 10.4271/2010-01-0511
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  3. Othmer, C. “A continuous adjoint formulation for the computation of topological and surface sensitivities of ducted flows,” Int. J. Num. Meth. Fluids 2007
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  8. Hill, D.C. “The Automatic Generation of Adjoint Solutions for a General Purpose Flow Solver” 46th AIAA Aerospace Sciences Meeting & Exhibit 7 10 January 2008 Reno, Nevada AIAA2008-0904

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