Continuous and discrete adjoint approaches for aerodynamic shape optimization with low Mach number preconditioning-Reference-Cited by-同舟云学术

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Continuous and discrete adjoint approaches for aerodynamic shape optimization with low Mach number preconditioning

Published:2008-08-10 Issue:10 Volume:57 Page:1485-1504
ISSN:0271-2091
Container-title:International Journal for Numerical Methods in Fluids
language:en
Short-container-title:Int. J. Numer. Meth. Fluids

Author:

Asouti V. G.,Zymaris A. S.,Papadimitriou D. I.,Giannakoglou K. C.

Publisher

Wiley

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1002/fld.1667/fullpdf

Reference31 articles.

1. Anderson WK, Newman JC, Whitfield DL, Nielsen EJ. Sensitivity analysis for the Navier–Stokes equations on unstructured meshes using complex variables. Fourteenth AIAA Computational Fluid Dynamics Conference, Norfolk, VA, AIAA Paper 1999‐3294, June 1999.

2. Nadarajah S, Jameson A. A comparison of the continuous and discrete adjoint approach to automatic aerodynamic optimization. Thirty‐eighth AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 2000‐0667, January 2000.

3. Optimal Shape Design for Elliptic Systems

4. Aerodynamic design via control theory;Jameson;Journal of Scientific Computing,1998

5. Jameson A. Optimum aerodynamic design using CFD and control theory. Twelfth AIAA Computational Fluid Dynamics Conference, San Diego, CA, AIAA Paper 1995‐1729, June 1995.

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