Abstract
In this research, the improvement of wind turbine blade undergoing pitching motion by means of identifying optimized aerofoil profile has been studied as a crucial part of enhancing effectiveness of wind energy turbine system. Here, the projected air is considered as unidirectional with flow speed range of Re 5*105 to 106. The effect of different pitching aerofoil blade profiles ranging from NACA 0012, S-809, and SD 7062 has been investigated in addition to the aerodynamic characteristics, entropy generation in the flow and exergy which are also proposed as a criterion for selecting optimum design for the oscillating aerofoil blade. Finally, increment in Re shows increase in the entropy generation rate and decrease in exergy efficiency. Consequently, aerofoil profile shows prominent variations in exergy with SD 7062 experiencing least entropy generation rate and exergy efficiency of around 93% due to its streamlined profile as compared to other profiles in this study. Meanwhile, NACA 0012 experiences minimum exergy efficiency of around 39% for Re 106.
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Abbreviations
- C:
-
Chord length [m]
- \({C}_{\mathrm{D}}\) :
-
Coefficient of drag
- \({C}_{\mathrm{L}}\) :
-
Coefficient of lift
- \(\dot{E}\) :
-
Exergy [W]
- \(I\) :
-
Irreversibility [W/m3]
- \({I}_{\mathrm{l}}\) :
-
Local entropy generation
- \(K\) :
-
Reduced frequency
- \(k\) :
-
Turbulence kinetic energy [m2/s2]
- \(P\) :
-
Pressure [Pa]
- \(\mathrm{Re}\) :
-
Reynolds number
- \({S}_{\mathrm{G}}\) :
-
Total entropy generation rate [W/K]
- \({S}_{\mathrm{gen}}\) :
-
Local entropy generation rate [W/(m3K)]
- \({S}_{x}\) :
-
Source term for body force-x
- \({S}_{y}\) :
-
Source term for body force-y
- \(t\) :
-
Flow time [s]
- \({T}_{0}\) :
-
Reference temperature [K]
- \(u\) :
-
Stream-wise velocity [m/s]
- \({u}_{\infty }\) :
-
Free-stream velocity [m/s]
- \(v\) :
-
Cross-stream velocity [m/s]
- \(x\) :
-
Stream-wise dimension of coordinates [m]
- \(y\) :
-
Cross-stream dimension of coordinates [m]
- y + :
-
Non-dimensional wall distance
- \(\alpha\) :
-
Angle of attack [deg]
- \({\alpha }_{\mathrm{mean}}\) :
-
Mean \(\alpha\) [deg]
- \({\alpha }_{\mathrm{amp}}\) :
-
Amplitude \(\alpha\) [deg]
- ϵ:
-
Turbulence dissipation rate [m2/s2]
- \(\rho\) :
-
Density of fluid [kgm−3]
- \({\tau }_{ij}\) :
-
Shear stress tensor
- \(\mu\) :
-
Viscosity of fluid [Pa s]
- \({\mu }_{t}\) :
-
Turbulent viscosity [Pa s]
- \(\omega\) :
-
Angular frequency [rad/s
- NACA:
-
National Advisory Committee for Aeronautics
- NREL:
-
National renewable energy laboratory
- SIMPLE:
-
Semi-implicit method for pressure-linked equations
- SST:
-
Shear stress transport
- NACA:
-
National Advisory Committee for Aeronautics
- NREL:
-
National renewable energy laboratory
- SIMPLE:
-
Semi-implicit method for pressure-linked equations
- SST:
-
Shear stress transport
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Acknowledgements
This research is supported by the Product Development Laboratory and the Computational Fluid Dynamics Laboratory of the SRM Institute of Science and Technology. These supports are gratefully acknowledged.
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Varakhedkar, A., Kumar, R.S. Numerical Modelling and Entropy Analysis of Pitching Aerofoil Under the Dynamic Stall. Arab J Sci Eng 48, 11333–11350 (2023). https://doi.org/10.1007/s13369-022-07424-x
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DOI: https://doi.org/10.1007/s13369-022-07424-x