Fast convergence of inviscid fluid dynamic design problems.

DOI10.1016/S0045-7930(01)00090-1zbMath1084.76548OpenAlexW2145907676MaRDI QIDQ1871598

Bernard Grossman, Andrea Dadone

Publication date: 4 May 2003

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

Full work available at URL: https://doi.org/10.1016/s0045-7930(01)00090-1

zbMATH Keywords

OptimizationInviscid flowsDirect designInverse design

Mathematics Subject Classification ID

Transonic flows (76H05) Finite volume methods applied to problems in fluid mechanics (76M12) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Related Items (3)

Aerodynamic shape optimization using first and second order adjoint and direct approaches ⋮ Continuous and discrete adjoint approaches for aerodynamic shape optimization with low Mach number preconditioning ⋮ A general use adjoint formulation for compressible and incompressible inviscid fluid dynamic optimization

Cites Work

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• A comparison of optimization-based approaches for a model computational aerodynamics design problem
• Supercritical wing sections II. A handbook
• Progressive optimization of inverse fluid dynamic design problems

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