Numerical Prediction of the Aerodynamics and Acoustics of a Tip Leakage Flow Using Large-Eddy Simulation
A Large-Eddy Simulation of the tip leakage flow of a single airfoil is carried out. The configuration consists of a non-rotating, isolated airfoil between two horizontal plates with a gap of 10 mm between the tip of the airfoil and the lower plate. The Mach number of the incoming flow is 0.2, and th...
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doaj-33677a1c3f344a21871e5952efe668892021-09-26T00:26:03ZengMDPI AGInternational Journal of Turbomachinery, Propulsion and Power2504-186X2021-07-016272710.3390/ijtpp6030027Numerical Prediction of the Aerodynamics and Acoustics of a Tip Leakage Flow Using Large-Eddy SimulationDavid Lamidel0Guillaume Daviller1Michel Roger2Hélène Posson3Ecole Centrale de Lyon, Universite de Lyon, CNRS, Universite Claude Bernard Lyon 1, INSA Lyon, LMFA, UMR 5509, 69130 Ecully, FranceCFD Team, CERFACS, 31057 Toulouse, FranceEcole Centrale de Lyon, Universite de Lyon, CNRS, Universite Claude Bernard Lyon 1, INSA Lyon, LMFA, UMR 5509, 69130 Ecully, FranceSafran Aircraft Engines, 77550 Moissy Cramayel, FranceA Large-Eddy Simulation of the tip leakage flow of a single airfoil is carried out. The configuration consists of a non-rotating, isolated airfoil between two horizontal plates with a gap of 10 mm between the tip of the airfoil and the lower plate. The Mach number of the incoming flow is 0.2, and the Reynolds number based on the chord is 9.3 × 10<inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><msup><mrow></mrow><mn>5</mn></msup></semantics></math></inline-formula>. The objective of the present study is to investigate the best way to compute both the aerodynamics and acoustics of the tip leakage flow. In particular, the importance of the inflow conditions on the prediction of the tip leakage vortex and the airfoil loading is underlined. On the other hand, the complex structure of the tip leakage vortex and its convection along the airfoil was recovered due to the use of a mesh adaptation based on the dissipation of the kinetic energy. Finally, the ability of the wall law to model the flow in the tip leakage flow region was proven in terms of wall pressure fluctuations and acoustics in the far-field.https://www.mdpi.com/2504-186X/6/3/27large-eddy simulationfan noisetip leakage flowtip clearance noise |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
David Lamidel Guillaume Daviller Michel Roger Hélène Posson |
spellingShingle |
David Lamidel Guillaume Daviller Michel Roger Hélène Posson Numerical Prediction of the Aerodynamics and Acoustics of a Tip Leakage Flow Using Large-Eddy Simulation International Journal of Turbomachinery, Propulsion and Power large-eddy simulation fan noise tip leakage flow tip clearance noise |
author_facet |
David Lamidel Guillaume Daviller Michel Roger Hélène Posson |
author_sort |
David Lamidel |
title |
Numerical Prediction of the Aerodynamics and Acoustics of a Tip Leakage Flow Using Large-Eddy Simulation |
title_short |
Numerical Prediction of the Aerodynamics and Acoustics of a Tip Leakage Flow Using Large-Eddy Simulation |
title_full |
Numerical Prediction of the Aerodynamics and Acoustics of a Tip Leakage Flow Using Large-Eddy Simulation |
title_fullStr |
Numerical Prediction of the Aerodynamics and Acoustics of a Tip Leakage Flow Using Large-Eddy Simulation |
title_full_unstemmed |
Numerical Prediction of the Aerodynamics and Acoustics of a Tip Leakage Flow Using Large-Eddy Simulation |
title_sort |
numerical prediction of the aerodynamics and acoustics of a tip leakage flow using large-eddy simulation |
publisher |
MDPI AG |
series |
International Journal of Turbomachinery, Propulsion and Power |
issn |
2504-186X |
publishDate |
2021-07-01 |
description |
A Large-Eddy Simulation of the tip leakage flow of a single airfoil is carried out. The configuration consists of a non-rotating, isolated airfoil between two horizontal plates with a gap of 10 mm between the tip of the airfoil and the lower plate. The Mach number of the incoming flow is 0.2, and the Reynolds number based on the chord is 9.3 × 10<inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><msup><mrow></mrow><mn>5</mn></msup></semantics></math></inline-formula>. The objective of the present study is to investigate the best way to compute both the aerodynamics and acoustics of the tip leakage flow. In particular, the importance of the inflow conditions on the prediction of the tip leakage vortex and the airfoil loading is underlined. On the other hand, the complex structure of the tip leakage vortex and its convection along the airfoil was recovered due to the use of a mesh adaptation based on the dissipation of the kinetic energy. Finally, the ability of the wall law to model the flow in the tip leakage flow region was proven in terms of wall pressure fluctuations and acoustics in the far-field. |
topic |
large-eddy simulation fan noise tip leakage flow tip clearance noise |
url |
https://www.mdpi.com/2504-186X/6/3/27 |
work_keys_str_mv |
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