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.
- 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:
- 1483769
- DOI:
- 10.21947/1483769
Citation Formats
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data. United States: N. p., 2020.
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. 2020.
"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:Fri Mar 27 00:00:00 EDT 2020
@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 = {2020},
month = {3}
}