Direct, adjoint and mixed approaches for the computation of Hessian in airfoil design problems-Reference-Cited by-同舟云学术

Direct, adjoint and mixed approaches for the computation of Hessian in airfoil design problems

Published:2008 Issue:10 Volume:56 Page:1929-1943
ISSN:0271-2091
Container-title:International Journal for Numerical Methods in Fluids
language:en
Short-container-title:Int. J. Numer. Meth. Fluids

Author:

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.1584/fullpdf

Reference26 articles.

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2. Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers

3. , . An adjoint method for the calculation of remote sensitivities in supersonic flow. AIAA 40th Aerospace Sciences Meeting and Exhibit, Reno NV, January 2002; AIAA-2002-0261.

4. , . Non-linear frequency domain based optimum shape design for unsteady three-dimensional flow. AIAA Paper 2002-2838, 2002.

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