Underlying data, figures and scripts of the publication: Wake Scaling of Actuator Discs in Different Aspect Ratios
Datacite citation style:
Fulvio Scarano; Simao Ferreira, Carlos; Huang, Ming; Andrea Sciacchitano (2021): Underlying data, figures and scripts of the publication: Wake Scaling of Actuator Discs in Different Aspect Ratios. Version 4. 4TU.ResearchData. dataset. https://doi.org/10.4121/12923897.v4
Other citation styles (APA, Harvard, MLA, Vancouver, Chicago, IEEE) available at Datacite
Dataset
choose version:
version 5 - 2022-11-04 (latest)
version 4 - 2021-10-15
version 3 - 2021-08-05
version 2 - 2021-07-06
version 1 - 2020-09-14
This online resource contains raw dataset, MATLAB scripts for some kinematic wake models, and underlying data for the rticle under revision, "Actuator disc diameter formulation for vertical-axis wind turbine kinematic wake modelling"
history
- 2020-09-14 first online
- 2021-10-15 published, posted
publisher
4TU.ResearchData
funding
- Delft University of Technology
- China scholarship council
organizations
TU Delft, Faculty of Aerospace Engineering, Department of Aerodynamics, Wind Energy, Flight Performance & Propulsion (AWEP)
DATA
files (55)
- 1,568 bytesMD5:
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README.md - 719 bytesMD5:
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BPA_HAWT.m - 866 bytesMD5:
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BPA_VAWT.m - 511,130 bytesMD5:
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fig10_Stream-wise velocity contours and in-plane velocity vectors pattern at four cross sections downstream of the circular actuator..png - 571,833 bytesMD5:
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fig11_Stream-wise velocity contours and in-plane velocity vectors at cross sections downstream of the square actuator..png - 852,684 bytesMD5:
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fig12_Stream-wise velocity contours and in-plane velocity vectors at cross sections downstream of the rectangular actuator.png - 179,927 bytesMD5:
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fig13Vorticity magnitude over four cross sections downstream of the circular actuator.png - 190,038 bytesMD5:
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fig14_Vorticity magnitude over four cross sections downstream of the square actuator.png - 190,869 bytesMD5:
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fig15_Vorticity magnitude contours over four cross sections downstream of the rectangular actuator..png - 21,197 bytesMD5:
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fig16_Comparison of averaged stream-wise velocity deficit along X direction for the circular actuator.png - 45,450 bytesMD5:
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fig17_Comparison of stream-wise velocity profiles at different downstream locations for the case of a circle actuator.png - 104,853 bytesMD5:
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fig18_Comparison of cross-section averaged stream-wise velocity deficit along X direction.png - 38,142 bytesMD5:
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fig19_Comparison of stream-wise velocity deficit averaged in upper half of the projected area along X direction (normalized by Deq).png - 479,155 bytesMD5:
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fig1_Schematic representation of a HAWT wake modelled according to Jensen (top), Larsen (middle) and the BPA (bottom), respectively. Colour-coded momentum deficit (blue fo.png - 32,065 bytesMD5:
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fig20_Comparison of stream-wise velocity deficit averaged in upper half of the projected area along X direction (normalized by D).png - 162,996 bytesMD5:
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fig21_Representation of the experimental data (stream-wise velocity profile along Z), when normalized by Deq. (Labels follow legend from figure 20).png - 163,164 bytesMD5:
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fig22_Representation of the experimental data (stream-wise velocity profile along Y), when normalized by Deq. (Labels follow legend from figure 20).png - 163,303 bytesMD5:
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fig23_Representation of the experimental data (stream-wise velocity profile along Z), when normalized by D. (Labels follow legend from figure 20).png - 146,524 bytesMD5:
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fig24_Representation of the experimental data (stream-wise velocity profile along Y), when normalized by D (Labels follow legend from figure 20).png - 159,478 bytesMD5:
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fig25_Representation of the experimental data (stream-wise velocity profile along Z), when X is normalized by D, and Z is normalized by H. (Labels follow legend from figur.png - 154,823 bytesMD5:
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fig26_Representation of the experimental data (stream-wise velocity profile along Y), when X is normalized by D, and Y is normalized by D. (Labels follow legend from figur.png - 126,869 bytesMD5:
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fig27_Colour contours of the time-averaged and normalized stream-wise velocity of the circular actuator in the XY-plane at ZD = 0. Measurements by planar (left) and roboti.png - 645,997 bytesMD5:
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fig2_Schematic plot of the Jensen-like rectangular wake characterisation based on both D and H (Abkar 2018), Deq (Shamsoddin & Porté-Agel, 2020) and D(present work).png - 485,465 bytesMD5:
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fig3_Geometrical details of circular, square and rectangular porous plates..png - 183,019 bytesMD5:
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fig4_Layout of experiments wind tunnel and square actuator at its exit. Robotic arm and coaxial volumetric velocimeter, with an indication of measurement region..png - 349,968 bytesMD5:
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fig5_Top- (up), and Front- (bottom) view of the porous plate (origin defined at the centre of the plate) and the IFOVs, the overall measurement domain is marked by the red.png - 194,449 bytesMD5:
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fig6_Raw (left) and pre-processed (right) CVV images of HFSB tracers, with the square actuator surface in view..png - 58,973 bytesMD5:
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fig7_Thrust coefficient as a function of porosity; comparison between current results and literature. .png - 147,909 bytesMD5:
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fig8_Contours of time-averaged and normalized stream-wise velocity in the XY-plane at ZD = 0. Circular (top), square (middle) and rectangular actuator (bottom)..png - 176,107 bytesMD5:
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fig9_Contours of time-averaged and normalized stream-wise velocity in the XZ-plane at YD = 0. Circular (top), square (middle) and rectangular actuator (bottom).png - 2,167,443 bytesMD5:
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Figure10_btm.dat - 2,258,886 bytesMD5:
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Figure10_mid.dat - 2,457,635 bytesMD5:
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Figure10_top.dat - 2,060,682 bytesMD5:
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Figure11.dat - 2,371,156 bytesMD5:
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Figure12.dat - 2,394,548 bytesMD5:
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Figure13.dat - 2,161,221 bytesMD5:
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Figure14.dat - 2,161,221 bytesMD5:
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Figure16.dat - 19,012 bytesMD5:
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Figure18.dat - 41,388 bytesMD5:
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Figure19.dat - 33,623 bytesMD5:
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Figure8.dat - 1,722,103 bytesMD5:
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Figure9_bottom.dat - 2,323,861 bytesMD5:
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Figure9_mid.dat - 1,994,131 bytesMD5:
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Figure9_top.dat - 432 bytesMD5:
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Jensen_HAWT.m - 648 bytesMD5:
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Jensen_VAWT.m - 772 bytesMD5:
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Larsen_HAWT.m - 54,544 bytesMD5:
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TurbulenceIntensity_IUXY.dat - 75,099 bytesMD5:
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TurbulenceIntensity_IUXY.png - 67,256 bytesMD5:
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TurbulenceIntensity_IUXZ.dat - 72,846 bytesMD5:
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TurbulenceIntensity_IUXZ.png -
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