Pages that link to "Item:Q5249452"
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The following pages link to Continuous and Discrete Adjoint Approach Based on Lattice Boltzmann Method in Aerodynamic Optimization Part I: Mathematical Derivation of Adjoint Lattice Boltzmann Equations (Q5249452):
Displaying 9 items.
- A comparison of the continuous and discrete adjoint approach extended based on the standard lattice Boltzmann method in flow field inverse optimization problems (Q293688) (← links)
- An adjoint-based lattice Boltzmann method for noise control problems (Q349510) (← links)
- Adjoint-based fluid flow control and optimisation with lattice Boltzmann methods (Q493491) (← links)
- Airfoil design optimization based on lattice Boltzmann method and adjoint approach (Q725227) (← links)
- Adjoint lattice Boltzmann equation for parameter identification (Q1043119) (← links)
- A novel approach of unsteady adjoint lattice Boltzmann method based on circular function scheme (Q2211750) (← links)
- Flow simulation around cambered airfoil by using conformal mapping and intermediate domain in lattice Boltzmann method (Q2396603) (← 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)
