Comparison and analysis of natural laminar flow airfoil shape optimization results at transonic regime with bumps and trailing edge devices solved by Pareto games and EAs

DOI10.1007/978-3-030-62543-6_4zbMath1502.65169OpenAlexW3144413145MaRDI QIDQ2050290

Yongbin Chen, Zhili Tang, Jacques Periaux

Publication date: 30 August 2021

Full work available at URL: https://doi.org/10.1007/978-3-030-62543-6_4

zbMATH Keywords

multi-objective optimizationevolutionary optimizationnatural laminar airfoilPareto gamesshock control bumptrailing edge device

Mathematics Subject Classification ID

Numerical optimization and variational techniques (65K10) Navier-Stokes equations for incompressible viscous fluids (76D05) Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05) Inverse problems for PDEs (35R30) Optimization of shapes other than minimal surfaces (49Q10) Numerical methods for partial differential equations, initial value and time-dependent initial-boundary value problems (65M99) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Cites Work

• Shooting and parallel shooting methods for solving the Falkner-Skan boundary layer equation
• The laminar generalized Stokes layer and turbulent drag reduction
• Unnamed Item

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