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UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data
**Overview**
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.
**Data Details**
File naming information can be found in the attached Word document "Sequence 6 Filename Key", copied from the Phase VI Test Report.
Complete Metadata
| @type | dcat:Dataset |
|---|---|
| accessLevel | public |
| bureauCode |
[
"019:20"
]
|
| contactPoint |
{
"fn": "Lee Fingersh",
"@type": "vcard:Contact",
"hasEmail": "mailto:lee.fingersh@nrel.gov"
}
|
| dataQuality |
true
|
| description | **Overview** 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. **Data Details** File naming information can be found in the attached Word document "Sequence 6 Filename Key", copied from the Phase VI Test Report. |
| distribution |
[
{
"@type": "dcat:Distribution",
"title": "uae6/uae6.z27.00",
"format": "00",
"accessURL": "https://a2e.energy.gov/data/uae6/uae6.z27.00",
"mediaType": "application/octet-stream",
"description": "Main dataset landing page with options to request/download"
}
]
|
| DOI | 10.21947/1483769 |
| identifier | https://data.openei.org/submissions/4193 |
| issued | 2018-11-29T00:00:00Z |
| keyword |
[
"00",
"Raw Data",
"Sequence 6",
"UAE6",
"Unsteady Aerodynamics Experiment Phase VI NREL-NASA Ames Wind Tunnel Experiment",
"Wind Tunnel Tests Data",
"a2e",
"atmosphere to electrons",
"eere",
"uae6",
"weto",
"wind",
"z27"
]
|
| landingPage | https://a2e.energy.gov/data/uae6/uae6.z27.00 |
| license | https://creativecommons.org/licenses/by/4.0/ |
| modified | 2020-03-27T00:00:00Z |
| programCode |
[
"019:010"
]
|
| projectNumber |
"67025"
|
| projectTitle | Wind Data Hub |
| publisher |
{
"name": "Wind Energy Technologies Office (WETO)",
"@type": "org:Organization"
}
|
| title | UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence 6 - Raw Data |
