UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 4 - Raw Data
**Overview**
Sequence 4: Static Pressure Calibration (P)
This test sequence used a downwind, teetered turbine with a 3.4° cone angle. The wind speed
ranged from 5 m/s to 25 m/s. Yaw angles of 0° to 30° were achieved. The blade tip pitch was 3°.
The rotor rotated at 72 RPM. Blade and probe pressure measurements were collected. A static
pitot probe was installed on a boom 2.3 m upwind of the nacelle at hub height and connected to
the reference side of the Mensor digital differential pressure transducer through the pneumatic
rotary coupling. This provided the reference pressure for all blade-mounted pressure transducers,
as opposed to the NASA atmospheric pressure reference that was used for all other test
sequences. This simulates the pressure system connections used in field measurements where the
static pressure was unknown.
**Data Details**
File naming information can be found in the attached Word document "Sequence 4 Filename Key", copied from the Phase VI Test Report.
Citation Formats
TY - DATA
AB - **Overview**
Sequence 4: Static Pressure Calibration (P)
This test sequence used a downwind, teetered turbine with a 3.4° cone angle. The wind speed
ranged from 5 m/s to 25 m/s. Yaw angles of 0° to 30° were achieved. The blade tip pitch was 3°.
The rotor rotated at 72 RPM. Blade and probe pressure measurements were collected. A static
pitot probe was installed on a boom 2.3 m upwind of the nacelle at hub height and connected to
the reference side of the Mensor digital differential pressure transducer through the pneumatic
rotary coupling. This provided the reference pressure for all blade-mounted pressure transducers,
as opposed to the NASA atmospheric pressure reference that was used for all other test
sequences. This simulates the pressure system connections used in field measurements where the
static pressure was unknown.
**Data Details**
File naming information can be found in the attached Word document "Sequence 4 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 - 10.21947/1483768
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 4
KW - Raw Data
KW - z25
KW - 00
LA - English
DA - 2018/11/29
PY - 2018
PB - Wind Energy Technologies Office (WETO)
T1 - UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 4 - Raw Data
UR - https://doi.org/10.21947/1483768
ER -
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 4 - Raw Data. Wind Energy Technologies Office (WETO), 29 November, 2018, A2E. https://doi.org/10.21947/1483768.
Fingersh, L. (2018). UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 4 - Raw Data. [Data set]. A2E. Wind Energy Technologies Office (WETO). https://doi.org/10.21947/1483768
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 4 - Raw Data. Wind Energy Technologies Office (WETO), November, 29, 2018. Distributed by A2E. https://doi.org/10.21947/1483768
@misc{OEDI_Dataset_4191,
title = {UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 4 - Raw Data},
author = {Fingersh, Lee},
abstractNote = {**Overview**
Sequence 4: Static Pressure Calibration (P)
This test sequence used a downwind, teetered turbine with a 3.4° cone angle. The wind speed
ranged from 5 m/s to 25 m/s. Yaw angles of 0° to 30° were achieved. The blade tip pitch was 3°.
The rotor rotated at 72 RPM. Blade and probe pressure measurements were collected. A static
pitot probe was installed on a boom 2.3 m upwind of the nacelle at hub height and connected to
the reference side of the Mensor digital differential pressure transducer through the pneumatic
rotary coupling. This provided the reference pressure for all blade-mounted pressure transducers,
as opposed to the NASA atmospheric pressure reference that was used for all other test
sequences. This simulates the pressure system connections used in field measurements where the
static pressure was unknown.
**Data Details**
File naming information can be found in the attached Word document "Sequence 4 Filename Key", copied from the Phase VI Test Report.},
url = {https://a2e.energy.gov/data/uae6/uae6.z25.00},
year = {2018},
howpublished = {A2E, Wind Energy Technologies Office (WETO), https://doi.org/10.21947/1483768},
note = {Accessed: 2025-05-28},
doi = {10.21947/1483768}
}
https://dx.doi.org/10.21947/1483768
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.z25.00Research 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 4, Raw Data, z25, 00DOE Project Details
Project Name Wind Data Hub
Project Number 67025
