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Title: UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence X - Raw Data

Abstract

Sequence X: Elevated RPM (F) This test sequence used an upwind, rigid turbine with a 0° cone angle. The wind speed ranged from 5 m/s to 12 m/s, and yaw angles of ±30° were obtained. The blade pitch angle was 3°. The rotor rotated at 90 RPM. Blade pressure measurements were collected. The five-hole probes were removed and the plugs were installed. Plastic tape 0.03-mm-thick was used to smooth the interface between the plugs and the blade. 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 load cell was pre-tensioned to 40,000 N. During post-processing, the probe channels were set to read -99999.99. As described in Appendix F, the hydrostatic correction derived for operation at 72 RPM was applied to these data.

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:
1483944
DOI:
10.21947/1483944

Citation Formats

Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence X - Raw Data. United States: N. p., 2019. Web. doi:10.21947/1483944.
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence X - Raw Data. United States. doi:10.21947/1483944.
Fingersh, Lee. 2019. "UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence X - Raw Data". United States. doi:10.21947/1483944. https://www.osti.gov/servlets/purl/1483944. Pub date:Wed Dec 11 00:00:00 EST 2019
@article{osti_1483944,
title = {UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence X - Raw Data},
author = {Fingersh, Lee},
abstractNote = {Sequence X: Elevated RPM (F) This test sequence used an upwind, rigid turbine with a 0° cone angle. The wind speed ranged from 5 m/s to 12 m/s, and yaw angles of ±30° were obtained. The blade pitch angle was 3°. The rotor rotated at 90 RPM. Blade pressure measurements were collected. The five-hole probes were removed and the plugs were installed. Plastic tape 0.03-mm-thick was used to smooth the interface between the plugs and the blade. 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 load cell was pre-tensioned to 40,000 N. During post-processing, the probe channels were set to read -99999.99. As described in Appendix F, the hydrostatic correction derived for operation at 72 RPM was applied to these data.},
doi = {10.21947/1483944},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2019},
month = {12}
}

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