Immersed boundary method on deformable unstructured meshes for airfoil aeroacoustic simulation

DOI10.1134/S0965542519120029zbMath1457.76090OpenAlexW3006975192MaRDI QIDQ2206386

L. N. Kudryavtseva, I. V. Abalakin, N. S. Zhdanova, Tatiana Kozubskaya, A. P. Duben'

Publication date: 22 October 2020

Published in: Computational Mathematics and Mathematical Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0965542519120029

zbMATH Keywords

turbulent flowmoving meshBrinkman penalization methodleading-edge slatLES approach

Mathematics Subject Classification ID

Direct numerical and large eddy simulation of turbulence (76F65) Hydro- and aero-acoustics (76Q05) Compressibility effects in turbulence (76F50)

Uses Software

• Spalart-Allmaras

Cites Work

• A penalization method to take into account obstacles in incompressible viscous flows
• Numerical investigation of the deflector effect on the aerodynamic and acoustic characteristics of turbulent cavity flow
• Hypoelastic stabilization of variational algorithm for construction of moving deforming meshes
• Variational method for untangling and optimization of spatial meshes
• Numerical Simulation of Flows over Moving Bodies of Complex Shapes Using Immersed Boundary Method on Unstructured Meshes
• Spalart-Allmaras

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