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Mathematical derivation of a unified equations for adjoint lattice Boltzmann method in airfoil and wing aerodynamic shape optimization - MaRDI portal

Mathematical derivation of a unified equations for adjoint lattice Boltzmann method in airfoil and wing aerodynamic shape optimization (Q6649202)

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scientific article; zbMATH DE number 7954649
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English
Mathematical derivation of a unified equations for adjoint lattice Boltzmann method in airfoil and wing aerodynamic shape optimization
scientific article; zbMATH DE number 7954649

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    Mathematical derivation of a unified equations for adjoint lattice Boltzmann method in airfoil and wing aerodynamic shape optimization (English)
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    5 December 2024
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    unified equations
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    aerodynamic shape optimization
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    continues adjoint method
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    lattice Boltzmann method
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    circular and spherical function
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