Towards Large Eddy Simulation of gas turbine compressors
W. A. McMullan,Gary J. Page +1 more
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TLDR
In this article, a series of simulations performed on compressor geometries, ranging from a Controlled Diffusion Cascade stator blade to the periodic sector of a stage in a 3.5 stage axial compressor, were presented.About:
This article is published in Progress in Aerospace Sciences.The article was published on 2012-07-01 and is currently open access. It has received 42 citations till now. The article focuses on the topics: Axial compressor & Gas compressor.read more
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An overset grid method for large eddy simulation of turbomachinery stages
Gaofeng Wang,Florent Duchaine,Dimitrios Papadogiannis,Ignacio Duran,Stéphane Moreau,Laurent Gicquel +5 more
TL;DR: A coupling method based on the overset grid approach has been successfully developed to couple multi-copies of a massively-parallel unstructured compressible LES solver AVBP for turbomachinery applications.
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Large eddy simulation of flows in industrial compressors: a path from 2015 to 2035
TL;DR: An overview of the current status of large eddy simulation for industrial compressor flows as well as to propose future research axes regarding the use of LES for compressor design are given.
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Numerical Investigation of Contrasting Flow Physics in Different Zones of a High-Lift Low Pressure Turbine Blade
TL;DR: In this paper, the effect of the state of the incoming boundary layer on flow features has been investigated on the suction surface, pressure surface, and endwalls of a low-pressure turbine blade.
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Future Use of Large Eddy Simulation in Aero‐engines
James Tyacke,Paul G. Tucker +1 more
TL;DR: In this article, a tentative expert system for industrial use of large-eddy simulation (LES) has been proposed, based on flow taxonomy, best practices including RANS/LES zonalization, meshing requirements, and turbulent inflow conditions.
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Prediction of the unsteady turbulent flow in an axial compressor stage. Part 1: Comparison of unsteady RANS and LES with experiments
TL;DR: In this paper, the capability of LES to predict the turbulent flow in a stage of an axial compressor and compare the results with unsteady RANS data and experiments is investigated.
References
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General circulation experiments with the primitive equations
TL;DR: In this article, an extended period numerical integration of a baroclinic primitive equation model has been made for the simulation and the study of the dynamics of the atmosphere's general circulation, and the solution corresponding to external gravitational propagation is filtered by requiring the vertically integrated divergence to vanish identically.
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On the identification of a vortex
Jinhee Jeong,Fazle Hussain +1 more
TL;DR: In this article, the authors propose a definition of vortex in an incompressible flow in terms of the eigenvalues of the symmetric tensor, which captures the pressure minimum in a plane perpendicular to the vortex axis at high Reynolds numbers, and also accurately defines vortex cores at low Reynolds numbers.
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Application of the energy-dissipation model of turbulence to the calculation of flow near a spinning disc
Brian Launder,B. I. Sharma +1 more
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Generation of Turbulent Inflow Data for Spatially-Developing Boundary Layer Simulations
TL;DR: In this article, a method for generating three-dimensional, time-dependent turbulent inflow data for simulations of complex spatially developing boundary layers is described, which is essentially a variant of the Spalart method, optimized so that an existing inflow?outflow code can be converted to an inflow-generation device through the addition of one simple subroutine.
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A digital filter based generation of inflow data for spatially developing direct numerical or large eddy simulations
TL;DR: In this article, the authors present a new approach for generating artificial velocity data which reproduces first and second order one point statistics as well as a locally given autocorrelation function.
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