Numerical simulation for 3D flow in flow channel of aeroengine turbine fan based on dimension splitting method

DOI10.3934/era.2020043zbMath1453.65327OpenAlexW3009474113MaRDI QIDQ779902

D. Kharzeev

Publication date: 14 July 2020

Published in: Electronic Research Archive (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.3934/era.2020043

zbMATH Keywords

aeroengine turbine fanrotational Navier-Stokes equationssemi-geodesic coordinate system

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) General theory of rotating fluids (76U05) Finite element, Rayleigh-Ritz and Galerkin methods for boundary value problems involving PDEs (65N30) Finite difference methods for initial value and initial-boundary value problems involving PDEs (65M06) Finite element, Rayleigh-Ritz and Galerkin methods for initial value and initial-boundary value problems involving PDEs (65M60) Numerical methods for inverse problems for initial value and initial-boundary value problems involving PDEs (65M32) Numerical methods for ill-posed problems for initial value and initial-boundary value problems involving PDEs (65M30) Compressible Navier-Stokes equations (76N06)

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Cites Work

• Unnamed Item
• An introduction to differential geometry with applications to elasticity
• Computational analysis of flow-driven string dynamics in turbomachinery
• A novel variational method for 3D viscous flow in flow channel of turbomachines based on differential geometry
• A Weak Galerkin Finite Element Method for the Navier-Stokes Equations
• Estimation of Impacts of Removing Arbitrarily Constrained Domain Details to the Analysis of Incompressible Fluid Flows

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