Incidence Angle Effect on the Behaviour of a Flow around the Turbine Blades

Our work involves a numerical simulation of a turbulent flow that crosses a turbine blade for different orientation angles using a computational fluid dynamics (CFD) code. The turbine's performance mainly depends on the characteristics and efficiency of the blades for optimal orientation angle position. The numerical simulation is based on the finite volume method for the differential equations discretization; different schemes have been used to solve these equations such as first upwind, second upwind, and power law. The turbulence model used in this study is the standard k-epsilon model. The equations governing the flow are solved by the Semi-Implicit Method for Pressure-linked Equations SIMPLE algorithm. The results obtained allow for identifying and characterizing the flow around the blade by plotting the dynamic field, the pressure coefficient, and the Mach number.

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Publication Details

Journal
WSEAS TRANSACTIONS ON FLUID MECHANICS
Published
2025-02-10
DOI
https://doi.org/10.37394/232013.2025.20.4
Citations
1
Primary Topic
Cyclone Separators and Fluid Dynamics
Type
article
Field-Weighted Citation Impact
1.33
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article

Incidence Angle Effect on the Behaviour of a Flow around the Turbine Blades

Merouane Habib, Rachid Sahnoun, Ismail Drai
1 citations
WSEAS TRANSACTIONS ON FLUID MECHANICS
Cyclone Separators and Fluid Dynamics
1.33
article

Incidence Angle Effect on the Behaviour of a Flow around the Turbine Blades

Merouane Habib, Rachid Sahnoun, Ismail Drai
article en
1 citations

Abstract

Our work involves a numerical simulation of a turbulent flow that crosses a turbine blade for different orientation angles using a computational fluid dynamics (CFD) code. The turbine's performance mainly depends on the characteristics and efficiency of the blades for optimal orientation angle position. The numerical simulation is based on the finite volume method for the differential equations discretization; different schemes have been used to solve these equations such as first upwind, second upwind, and power law. The turbulence model used in this study is the standard k-epsilon model. The equations governing the flow are solved by the Semi-Implicit Method for Pressure-linked Equations SIMPLE algorithm. The results obtained allow for identifying and characterizing the flow around the blade by plotting the dynamic field, the pressure coefficient, and the Mach number.

WSEAS TRANSACTIONS ON FLUID MECHANICSVol. 20
Université Mustapha Stambouli de Mascara (DZ)
Openalex Percentile: Top 27%
Cyclone Separators and Fluid Dynamics
1.33
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