UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence D - Raw Data
Abstract
Sequences B, C, and D: Downwind Baseline (F), Downwind Low Pitch (F), Downwind High Pitch (F) 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 ±180° were achieved at low wind speeds, and yaw angles of -20° to 10° were achieved for high wind speeds. The blade tip pitch was 3° for sequence B, 0° for sequence C, and 6° for sequence D. These three sequences were interleaved during testing because the pitch angle change was easily made by the turbine operator. The rotor rotated at 72 RPM. Blade and probe pressure measurements were collected.
- Authors:
- Publication Date:
- DOE Contract Number:
- 67025F
- Product Type:
- Dataset
- Research Org.:
- Pacific Northwest National Lab. (PNNL), Richland, WA (United States). Atmosphere to Electrons (A2e) Data Archive and Portal
- Sponsoring Org.:
- USDOE Office of Energy Efficiency and Renewable Energy (EERE), Wind and Water Technologies Office (EE-4W)
- Subject:
- 17 Wind Energy
- OSTI Identifier:
- 1482206
- DOI:
- 10.21947/1482206
Citation Formats
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence D - Raw Data. United States: N. p., 2020.
Web. doi:10.21947/1482206.
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence D - Raw Data. United States. doi:10.21947/1482206.
Fingersh, Lee. 2020.
"UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence D - Raw Data". United States. doi:10.21947/1482206. https://www.osti.gov/servlets/purl/1482206. Pub date:Fri Mar 27 00:00:00 EDT 2020
@article{osti_1482206,
title = {UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence D - Raw Data},
author = {Fingersh, Lee},
abstractNote = {Sequences B, C, and D: Downwind Baseline (F), Downwind Low Pitch (F), Downwind High Pitch (F) 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 ±180° were achieved at low wind speeds, and yaw angles of -20° to 10° were achieved for high wind speeds. The blade tip pitch was 3° for sequence B, 0° for sequence C, and 6° for sequence D. These three sequences were interleaved during testing because the pitch angle change was easily made by the turbine operator. The rotor rotated at 72 RPM. Blade and probe pressure measurements were collected.},
doi = {10.21947/1482206},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2020},
month = {3}
}
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