A Preconditioning Method for Shape Optimization Governed by the Euler Equations
作者:
EYAL ARIAN,
VEERN. VATSA,
期刊:
International Journal of Computational Fluid Dynamics
(Taylor Available online 1999)
卷期:
Volume 12,
issue 1
页码: 17-27
ISSN:1061-8562
年代: 1999
DOI:10.1080/10618569908940813
出版商: Taylor & Francis Group
关键词: Airfoil oplimization;Euler;optimal shape;preconditioning
数据来源: Taylor
摘要:
We consider a classical aerodynamic shape optimization problem subject to the compressible Euler flow equations. The gradient of the cost functional with respect to the shape variables is derived with the adjoint method at the continuous level. The Hessian (second order derivative of Ihe cost functional with respect to the shape variables) is approximated also at the continuous level, as first introduced by Arian and Ta'asan [1], The approximation of the Hessian is used to approximate the Newton step which is essential to accelerate the numerical solution of the optimization problem. The design space is discretized in the maximum dimension, i.e., the location of each point on the intersection of the computational mesh with the airfoil is taken to be an independent design variable. We give numerical examples for 86 design variables in two different flow speeds and achieve an order of magnitude reduction in the cost functional at a computational effort of a full solution of the analysis partial differential equation (PDE).
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