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Title: UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data

Abstract

Sequence 6: Shroud Wake Measure (P) This test sequence used a downwind, rigid turbine with a 3.4° cone angle. The wind speeds for this sequence corresponded to subcritical [7 m/s], transitional [15 m/s], and supercritical [20 m/s] Reynolds number regimes for the circular cross-section tower. The yaw angle and blade tip pitch angles were selected to traverse the probe tip across the tower wake while keeping the probe axis approximately parallel to the tunnel centerline. The rotor was parked with the instrumented blade at 180° azimuth. Blade and probe pressure measurements were collected. An airfoil-shaped aluminum shroud was placed on the tower below the 34% span five-hole probe. It extended below the 91% span five-hole probe. The turntable angle was adjusted to position the shroud at various angles relative to the flow.

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:
1483769
DOI:
10.21947/1483769

Citation Formats

Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data. United States: N. p., 2019. Web. doi:10.21947/1483769.
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data. United States. doi:10.21947/1483769.
Fingersh, Lee. 2019. "UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data". United States. doi:10.21947/1483769. https://www.osti.gov/servlets/purl/1483769. Pub date:Wed Dec 11 00:00:00 EST 2019
@article{osti_1483769,
title = {UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data},
author = {Fingersh, Lee},
abstractNote = {Sequence 6: Shroud Wake Measure (P) This test sequence used a downwind, rigid turbine with a 3.4° cone angle. The wind speeds for this sequence corresponded to subcritical [7 m/s], transitional [15 m/s], and supercritical [20 m/s] Reynolds number regimes for the circular cross-section tower. The yaw angle and blade tip pitch angles were selected to traverse the probe tip across the tower wake while keeping the probe axis approximately parallel to the tunnel centerline. The rotor was parked with the instrumented blade at 180° azimuth. Blade and probe pressure measurements were collected. An airfoil-shaped aluminum shroud was placed on the tower below the 34% span five-hole probe. It extended below the 91% span five-hole probe. The turntable angle was adjusted to position the shroud at various angles relative to the flow.},
doi = {10.21947/1483769},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2019},
month = {12}
}

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