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
Wind Energy Technologies Office (WETO). (2018). UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 4 - Raw Data [data set]. Retrieved from https://dx.doi.org/10.21947/1483768.
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 4 - Raw Data. United States: N.p., 29 Nov, 2018. Web. doi: 10.21947/1483768.
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 4 - Raw Data. United States. https://dx.doi.org/10.21947/1483768
Fingersh, Lee. 2018. "UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 4 - Raw Data". United States. https://dx.doi.org/10.21947/1483768. https://a2e.energy.gov/data/uae6/uae6.z25.00.
@div{oedi_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.}, doi = {10.21947/1483768}, url = {https://a2e.energy.gov/data/uae6/uae6.z25.00}, journal = {}, number = , volume = , place = {United States}, year = {2018}, month = {11}}
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
