Simulation of airflow past a 2D NACA0015 airfoil using an isogeometric incompressible Navier-Stokes solver with the Spalart-Allmaras turbulence model

DOI10.1016/J.CMA.2015.02.030zbMath1423.76184OpenAlexW2053121405MaRDI QIDQ1734466

Runar Holdahl, Knut Nordanger, Arne Morten Kvarving, Adil Rasheed, Trond Kvamsdal

Publication date: 27 March 2019

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.cma.2015.02.030

zbMATH Keywords

isogeometric analysisSpalart-Allmaraschorin projection methodNACA0015 airfoil

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) General aerodynamics and subsonic flows (76G25)

Related Items (4)

An upwind local radial basis functions-differential quadrature (RBF-DQ) method with proper orthogonal decomposition (POD) approach for solving compressible Euler equation ⋮ Hybrid analysis and modeling, eclecticism, and multifidelity computing toward digital twin revolution ⋮ Generalized weak Galerkin methods for Stokes equations ⋮ On the application of isogeometric finite volume method in numerical analysis of wet-steam flow through turbine cascades

Uses Software

• Trilinos
• Spalart-Allmaras

Cites Work

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• 3D simulation of wind turbine rotors at full scale. Part I: Geometry modeling and aerodynamics
• 3D simulation of wind turbine rotors at full scale. Part II: Fluid-structure interaction modeling with composite blades
• An overview of the Trilinos project
• Isogeometric Analysis
• On the error estimates for the rotational pressure-correction projection methods
• SPACE–TIME VMS METHODS FOR MODELING OF INCOMPRESSIBLE FLOWS AT HIGH REYNOLDS NUMBERS
• Numerical Solution of the Navier-Stokes Equations
• AN APPROXIMATE PROJECTION SCHEME FOR INCOMPRESSIBLE FLOW USING SPECTRAL ELEMENTS

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