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Title: 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.

Creator(s)/Author(s):
Publication Date:
DOE Contract Number:  
67025F
Product Type:
Dataset
Research Org.:
Atmosphere to Electrons (A2e) Data Archive and Portal, Pacific Northwest National Laboratory; PNNL
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., 2019. 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. 2019. "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:Wed Dec 11 00:00:00 EST 2019
@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 = {2019},
month = {12}
}

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