Design optimization of unsteady airfoils with continuous adjoint method

DOI10.1007/s10483-015-2010-9zbMath1326.76013OpenAlexW1193574193MaRDI QIDQ895314

Liang Fang, Xiao-Wei Li

Publication date: 27 November 2015

Published in: AMM. Applied Mathematics and Mechanics. (English Edition) (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10483-015-2010-9

zbMATH Keywords

unsteady flowcontinuous adjoint methodairfoil optimization

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10) Flow control and optimization for incompressible inviscid fluids (76B75)

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Cites Work

• Optimal aerodynamic design of airfoils in unsteady viscous flows
• Aerodynamic design via control theory
• Optimum aerodynamic design using the Navier-Stokes equations
• Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation
• Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers

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