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Synthetic turbulence generation for high-order scale-resolving simulations on unstructured grids
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![]() | Accepted version | 13.54 MB | Adobe PDF | View/Open |
Title: | Synthetic turbulence generation for high-order scale-resolving simulations on unstructured grids |
Authors: | Giangaspero, G Witherden, F Vincent, P |
Item Type: | Journal Article |
Abstract: | An extended version of the synthetic eddy method for generation of synthetic turbulence has been developed via a source term formulation and implemented in the open-source cross-platform solver PyFR. The method caters for the full space-dependent anisotropy of the target turbulent length scales, and it is agnostic of the space and time discretization of the underlying solver, which can be incompressible or compressible. Moreover, the method does not require each solution point to communicate with nearest neighbors; thus, it is well suited for modern, massively parallel, high-order unstructured codes which support mixed and possibly curved elements. The method has been applied to two test cases: incompressible plane channel flow at Reτ 180 and compressible flow over an SD7003 aerofoil at Re 66;000, Ma 0.2, and α 4 deg. The channel flow case was run on three topologically different meshes composed of hexahedra, prisms, and a combination of prisms and tetrahedra, respectively. Almost identical results have been obtained on the three meshes. Results also show that taking into account the anisotropy of the turbulent length scales can reduce the development length. For the SD7003 aerofoil case, the injection of synthetic turbulence improves agreement between numerical and experimental results. |
Issue Date: | 1-Feb-2022 |
Date of Acceptance: | 21-Aug-2021 |
URI: | http://hdl.handle.net/10044/1/92903 |
DOI: | 10.2514/1.J061046 |
ISSN: | 0001-1452 |
Publisher: | American Institute of Aeronautics and Astronautics |
Start Page: | 1032 |
End Page: | 1051 |
Journal / Book Title: | AIAA Journal: devoted to aerospace research and development |
Volume: | 60 |
Issue: | 2 |
Copyright Statement: | Copyright © 2021 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp |
Sponsor/Funder: | Engineering & Physical Science Research Council (EPSRC) |
Funder's Grant Number: | EP/R030340/1 |
Keywords: | Science & Technology Technology Engineering, Aerospace Engineering Isotropic Turbulence Unstructured Grid Incompressible Flow Aerofoil Boundary Layer Transition Direct Numerical Simulation Reynolds Averaged Navier Stokes Power Spectral Density Finite Element Scheme Kinematic Viscosity DIRECT NUMERICAL-SIMULATION LAMINAR SEPARATION-BUBBLES LARGE-EDDY SIMULATIONS INFLOW CONDITIONS CHANNEL FLOW BOUNDARY-LAYER Science & Technology Technology Engineering, Aerospace Engineering Isotropic Turbulence Unstructured Grid Incompressible Flow Aerofoil Boundary Layer Transition Direct Numerical Simulation Reynolds Averaged Navier Stokes Power Spectral Density Finite Element Scheme Kinematic Viscosity DIRECT NUMERICAL-SIMULATION LAMINAR SEPARATION-BUBBLES LARGE-EDDY SIMULATIONS INFLOW CONDITIONS CHANNEL FLOW BOUNDARY-LAYER Aerospace & Aeronautics 0901 Aerospace Engineering 0905 Civil Engineering 0913 Mechanical Engineering |
Publication Status: | Published |
Online Publication Date: | 2021-11-05 |
Appears in Collections: | Aeronautics Faculty of Engineering |