scispace - formally typeset
Open AccessJournal ArticleDOI

Towards Large Eddy Simulation of gas turbine compressors

Reads0
Chats0
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

Citations
More filters
Journal ArticleDOI

An overset grid method for large eddy simulation of turbomachinery stages

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.
Journal ArticleDOI

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.
Journal ArticleDOI

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.
Journal ArticleDOI

Future Use of Large Eddy Simulation in Aero‐engines

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.
Journal ArticleDOI

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
More filters
Journal ArticleDOI

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.
Journal ArticleDOI

On the identification of a vortex

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.
Journal ArticleDOI

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.
Journal ArticleDOI

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.
Trending Questions (1)
What type of combustion chamber is commonly used in axial compressor engines?

A recycling method is developed that improves the quality of the flow in a single stage calculation of an axial compressor, and indicates that future developments in both the recycling technique and computing power will bring simulations of axial compressors within reach of industry in the coming years.