Pages that link to "Item:Q725227"
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The following pages link to Airfoil design optimization based on lattice Boltzmann method and adjoint approach (Q725227):
Displaying 6 items.
- Open-loop optimal control of a flapping wing using an adjoint lattice Boltzmann method (Q2192531) (← links)
- A novel approach of unsteady adjoint lattice Boltzmann method based on circular function scheme (Q2211750) (← links)
- An interpolation-based lattice Boltzmann method for non-conforming orthogonal meshes (Q2234862) (← links)
- Continuous and Discrete Adjoint Approach Based on Lattice Boltzmann Method in Aerodynamic Optimization Part I: Mathematical Derivation of Adjoint Lattice Boltzmann Equations (Q5249452) (← links)
- Airfoil inverse design based on laminar compressible adjoint lattice Oltzmann method (Q6537478) (← links)
- Mathematical derivation of a unified equations for adjoint lattice Boltzmann method in airfoil and wing aerodynamic shape optimization (Q6649202) (← links)