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Published in:
On Scale Separation in Large Eddy Simulations Read chapter Read first chapter

2015 | OriginalPaper | Chapter

Compressible DNS of a Low Pressure Turbine Subjected to Inlet Disturbances

Authors : L. W. Chen, R. Pichler, R. D. Sandberg

Published in: Direct and Large-Eddy Simulation IX

Publisher: Springer International Publishing

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Abstract

In modern low pressure turbines (LPT), reducing the number of airfoils in a turbine leads to an increase in the blade loading, which inevitably increases the possibility of laminar separation.

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previous chapter Unsteady Characteristic of Stall Around an Airfoil by Means of High Fidelity LES
next chapter Large Eddy Simulation of a NACA-0012 Airfoil Near Stall
Literature
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Metadata
Title
Compressible DNS of a Low Pressure Turbine Subjected to Inlet Disturbances
Authors
L. W. Chen
R. Pichler
R. D. Sandberg
Copyright Year
2015
Book
Direct and Large-Eddy Simulation IX

Print ISBN: 978-3-319-14447-4

Electronic ISBN: 978-3-319-14448-1

Copyright Year: 2015

DOI
https://doi.org/10.1007/978-3-319-14448-1_48

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