UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence F - Raw Data
**Overview**
Sequence F: Downwind High Cone (F)
This test sequence used a downwind, rigid turbine with an 18° cone angle. The wind speed
ranged from 10 m/s to 20 m/s. Excessive inertial loading due to the high cone angle prevented
operation at lower wind speeds. Yaw angles of ±20° were achieved. The blade tip pitch was 3°.
The rotor rotated at 72 RPM. Blade and probe pressure measurements were collected. The teeter
dampers were replaced with rigid links, and these two channels were flagged as not applicable by
setting the measured values in the data file to ?99999.99 Nm. The teeter link was replaced with a
shorter bar so the load cell was not installed during this test. However, the teeter link load cell channel was flagged as not applicable by setting the measured values in the data file to
-99999.99 N.
**Data Details**
File naming information can be found in the attached Word document "Sequence F Filename Key", copied from the Phase VI Test Report.
Citation Formats
Wind Energy Technologies Office (WETO). (2018). UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence F - Raw Data [data set]. Retrieved from https://dx.doi.org/10.21947/1483641.
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence F - Raw Data. United States: N.p., 28 Nov, 2018. Web. doi: 10.21947/1483641.
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence F - Raw Data. United States. https://dx.doi.org/10.21947/1483641
Fingersh, Lee. 2018. "UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence F - Raw Data". United States. https://dx.doi.org/10.21947/1483641. https://a2e.energy.gov/data/uae6/uae6.z05.00.
@div{oedi_4201, title = {UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence F - Raw Data}, author = {Fingersh, Lee.}, abstractNote = {**Overview**
Sequence F: Downwind High Cone (F)
This test sequence used a downwind, rigid turbine with an 18° cone angle. The wind speed
ranged from 10 m/s to 20 m/s. Excessive inertial loading due to the high cone angle prevented
operation at lower wind speeds. Yaw angles of ±20° were achieved. The blade tip pitch was 3°.
The rotor rotated at 72 RPM. Blade and probe pressure measurements were collected. The teeter
dampers were replaced with rigid links, and these two channels were flagged as not applicable by
setting the measured values in the data file to ?99999.99 Nm. The teeter link was replaced with a
shorter bar so the load cell was not installed during this test. However, the teeter link load cell channel was flagged as not applicable by setting the measured values in the data file to
-99999.99 N.
**Data Details**
File naming information can be found in the attached Word document "Sequence F Filename Key", copied from the Phase VI Test Report.}, doi = {10.21947/1483641}, url = {https://a2e.energy.gov/data/uae6/uae6.z05.00}, journal = {}, number = , volume = , place = {United States}, year = {2018}, month = {11}}
https://dx.doi.org/10.21947/1483641
Details
Data from Nov 28, 2018
Last updated Mar 27, 2020
Submitted Nov 28, 2018
Organization
Wind Energy Technologies Office (WETO)
Contact
Lee Fingersh
303.384.6929
Authors
Original Source
https://a2e.energy.gov/data/uae6/uae6.z05.00Research 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 F, Raw Data, z05, 00DOE Project Details
Project Name Wind Data Hub
Project Number 67025
