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Direct numerical simulation of installation effects on airfoil noise
Ziyang Zhou
, Stéphane Moreau
,
Marlène Sanjosé
École de technologie supérieure
Aerospatial Engineering Department
TFT - Thermofluid Transport Laboratory
Université de Sherbrooke
Research output
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Contribution to journal
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Journal Article
›
peer-review
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Dive into the research topics of 'Direct numerical simulation of installation effects on airfoil noise'. Together they form a unique fingerprint.
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Keyphrases
Direct numerical Simulation
100%
Installation Effects
100%
Airfoil Noise
100%
Airfoil
66%
Angle of Attack
66%
Wind Tunnel
66%
Jet Shear Layer
66%
Shape Factor
33%
Trailing Edge
33%
Stress Magnitude
33%
Lattice Boltzmann Method
33%
Momentum Thickness
33%
Reynolds number
33%
Shear Layer
33%
Boundary Layer
33%
Operating State
33%
Controlled Diffusion Airfoil
33%
Power Flow
33%
Wall Pressure
33%
Far-field Noise
33%
Reynolds Stress
33%
Mixing Layer
33%
Trailing Edge Noise
33%
Mid-frequency Range
33%
Velocity Statistics
33%
Noise Generation
33%
Nozzle Lip
33%
Layer Refinement
33%
Boundary Layer Displacement Thickness
33%
Simulation Simulation
33%
Thickness Factor
33%
Physics
Airfoil
100%
Direct Numerical Simulation
100%
Shear Layer
75%
Wind Tunnel
50%
Boundary Layer
50%
Angle of Attack
50%
Lattice-Boltzmann Method
25%
Reynolds Number
25%
Far Field
25%
Wall Pressure
25%