A surrogate-model based multidisciplinary shape optimization method with application to a 2D subsonic airfoil

DOI10.1016/j.compfluid.2006.04.001zbMath1177.76367OpenAlexW2021830957MaRDI QIDQ1043222

J. Laurenceau, Pierre Sagaut, Jean-Christophe Jouhaud, Marc Montagnac

Publication date: 7 December 2009

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2006.04.001

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) General aerodynamics and subsonic flows (76G25) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Related Items (11)

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Uses Software

• LAPACK

Cites Work

• Unnamed Item
• Knowledge incorporation in evolutionary computation
• Design and analysis of computer experiments. With comments and a rejoinder by the authors
• Optimal aeroacoustic shape design using the surrogate management framework
• LAPACK Users' Guide
• Simulation of Transition with a Two-Equation Turbulence Model
• A multigrid adaptive mesh refinement strategy for 3D aerodynamic design

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