UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data
**Overview**
Sequence 6: Shroud Wake Measure (P)
This test sequence used a downwind, rigid turbine with a 3.4° cone angle. The wind speeds for
this sequence corresponded to subcritical [7 m/s], transitional [15 m/s], and supercritical [20 m/s]
Reynolds number regimes for the circular cross-section tower. The yaw angle and blade tip pitch
angles were selected to traverse the probe tip across the tower wake while keeping the probe axis
approximately parallel to the tunnel centerline. The rotor was parked with the instrumented blade
at 180° azimuth. Blade and probe pressure measurements were collected.
An airfoil-shaped aluminum shroud was placed on the tower below the 34% span five-hole probe. It
extended below the 91% span five-hole probe. The turntable angle was adjusted to position the
shroud at various angles relative to the flow.
**Data Details**
File naming information can be found in the attached Word document "Sequence 6 Filename Key", copied from the Phase VI Test Report.
Citation Formats
TY - DATA
AB - **Overview**
Sequence 6: Shroud Wake Measure (P)
This test sequence used a downwind, rigid turbine with a 3.4° cone angle. The wind speeds for
this sequence corresponded to subcritical [7 m/s], transitional [15 m/s], and supercritical [20 m/s]
Reynolds number regimes for the circular cross-section tower. The yaw angle and blade tip pitch
angles were selected to traverse the probe tip across the tower wake while keeping the probe axis
approximately parallel to the tunnel centerline. The rotor was parked with the instrumented blade
at 180° azimuth. Blade and probe pressure measurements were collected.
An airfoil-shaped aluminum shroud was placed on the tower below the 34% span five-hole probe. It
extended below the 91% span five-hole probe. The turntable angle was adjusted to position the
shroud at various angles relative to the flow.
**Data Details**
File naming information can be found in the attached Word document "Sequence 6 Filename Key", copied from the Phase VI Test Report.
AU - Fingersh, Lee
DB - Open Energy Data Initiative (OEDI)
DP - Open EI | National Renewable Energy Laboratory
DO - 10.21947/1483769
KW - a2e
KW - atmosphere to electrons
KW - wind
KW - weto
KW - eere
KW - uae6
KW - Unsteady Aerodynamics Experiment Phase VI NREL-NASA Ames Wind Tunnel Experiment
KW - UAE6
KW - Wind Tunnel Tests Data
KW - Sequence 6
KW - Raw Data
KW - z27
KW - 00
LA - English
DA - 2018/11/29
PY - 2018
PB - Wind Energy Technologies Office (WETO)
T1 - UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data
UR - https://doi.org/10.21947/1483769
ER -
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data. Wind Energy Technologies Office (WETO), 29 November, 2018, A2E. https://doi.org/10.21947/1483769.
Fingersh, L. (2018). UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data. [Data set]. A2E. Wind Energy Technologies Office (WETO). https://doi.org/10.21947/1483769
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data. Wind Energy Technologies Office (WETO), November, 29, 2018. Distributed by A2E. https://doi.org/10.21947/1483769
@misc{OEDI_Dataset_4193,
title = {UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data},
author = {Fingersh, Lee},
abstractNote = {**Overview**
Sequence 6: Shroud Wake Measure (P)
This test sequence used a downwind, rigid turbine with a 3.4° cone angle. The wind speeds for
this sequence corresponded to subcritical [7 m/s], transitional [15 m/s], and supercritical [20 m/s]
Reynolds number regimes for the circular cross-section tower. The yaw angle and blade tip pitch
angles were selected to traverse the probe tip across the tower wake while keeping the probe axis
approximately parallel to the tunnel centerline. The rotor was parked with the instrumented blade
at 180° azimuth. Blade and probe pressure measurements were collected.
An airfoil-shaped aluminum shroud was placed on the tower below the 34\% span five-hole probe. It
extended below the 91\% span five-hole probe. The turntable angle was adjusted to position the
shroud at various angles relative to the flow.
**Data Details**
File naming information can be found in the attached Word document "Sequence 6 Filename Key", copied from the Phase VI Test Report.},
url = {https://a2e.energy.gov/data/uae6/uae6.z27.00},
year = {2018},
howpublished = {A2E, Wind Energy Technologies Office (WETO), https://doi.org/10.21947/1483769},
note = {Accessed: 2025-05-28},
doi = {10.21947/1483769}
}
https://dx.doi.org/10.21947/1483769
Details
Data from Nov 29, 2018
Last updated Mar 27, 2020
Submitted Nov 29, 2018
Organization
Wind Energy Technologies Office (WETO)
Contact
Lee Fingersh
303.384.6929
Authors
Original Source
https://a2e.energy.gov/data/uae6/uae6.z27.00Research Areas
Keywords
a2e, atmosphere to electrons, wind, weto, eere, uae6, Unsteady Aerodynamics Experiment Phase VI NREL-NASA Ames Wind Tunnel Experiment, UAE6, Wind Tunnel Tests Data, Sequence 6, Raw Data, z27, 00DOE Project Details
Project Name Wind Data Hub
Project Number 67025
