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UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence N - Raw Data

Publicly accessible License 

**Overview**

Sequence N: Sin AOA, Rotating (P)

This sequence was designed to quantify the blade 3-D unsteady aerodynamic response in the
presence of rotational influences by varying blade pitch angle. Test sequence N used an upwind,
rigid turbine with a 0° cone angle. The wind speed was 15 m/s, and the yaw angle was 0°
throughout the sequence. The rotor rotated at 72 RPM. Blade and probe pressure measurements
were collected. 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.

Sinusoidal angle-of-attack histories were designed to emulate 2-D S809 dynamic data obtained at
the Ohio State University (OSU) wind tunnel (Reuss Ramsey et al. 1995) and the 1P yawed flow
angle-of-attack variations the turbine could be expected to encounter in routine operation. The
reduced frequency (K), mean angle of attack (?m), and oscillation amplitude (??) were computed
for each of the five primary span locations. The file lengths varied according to the time required
to complete 40 oscillations at the specified frequency. The file name convention used the
sequence designation N, followed by two digits for the span location (30, 47, 63, 80, or 95),
followed by two digits representing the condition specified in the test matrix, followed by the
repetition digit. Due to time constraints, most of the test conditions corresponding to the 63%
span location were eliminated. Test points with a
static pitch angle of 3° were collected throughout the sequence to ascertain instrumentation fidelity.

**Data Details**

File naming information can be found in the attached Word document "Sequence N Filename Key", copied from the Phase VI Test Report.

Citation Formats

TY - DATA AB - **Overview** Sequence N: Sin AOA, Rotating (P) This sequence was designed to quantify the blade 3-D unsteady aerodynamic response in the presence of rotational influences by varying blade pitch angle. Test sequence N used an upwind, rigid turbine with a 0° cone angle. The wind speed was 15 m/s, and the yaw angle was 0° throughout the sequence. The rotor rotated at 72 RPM. Blade and probe pressure measurements were collected. 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. Sinusoidal angle-of-attack histories were designed to emulate 2-D S809 dynamic data obtained at the Ohio State University (OSU) wind tunnel (Reuss Ramsey et al. 1995) and the 1P yawed flow angle-of-attack variations the turbine could be expected to encounter in routine operation. The reduced frequency (K), mean angle of attack (αm), and oscillation amplitude (αω) were computed for each of the five primary span locations. The file lengths varied according to the time required to complete 40 oscillations at the specified frequency. The file name convention used the sequence designation N, followed by two digits for the span location (30, 47, 63, 80, or 95), followed by two digits representing the condition specified in the test matrix, followed by the repetition digit. Due to time constraints, most of the test conditions corresponding to the 63% span location were eliminated. Test points with a static pitch angle of 3° were collected throughout the sequence to ascertain instrumentation fidelity. **Data Details** File naming information can be found in the attached Word document "Sequence N Filename Key", copied from the Phase VI Test Report. AU - Fingersh, Lee DB - Open Energy Data Initiative (OEDI) DP - Open EI | National Renewable Energy Laboratory DO - 10.21947/1483820 KW - a2e KW - atmosphere to electrons KW - wind KW - weto KW - eere KW - uae6 KW - Unsteady Aerodynamics Experiment Phase VI NREL-NASA Ames Wind Tunnel Experiment KW - UAE6 KW - Wind Tunnel Tests Data KW - Sequence N KW - Raw Data KW - z13 KW - 00 LA - English DA - 2018/11/29 PY - 2018 PB - Wind Energy Technologies Office (WETO) T1 - UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence N - Raw Data UR - https://doi.org/10.21947/1483820 ER -
Export Citation to RIS
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence N - Raw Data. Wind Energy Technologies Office (WETO), 29 November, 2018, A2E. https://doi.org/10.21947/1483820.
Fingersh, L. (2018). UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence N - Raw Data. [Data set]. A2E. Wind Energy Technologies Office (WETO). https://doi.org/10.21947/1483820
Fingersh, Lee. UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence N - Raw Data. Wind Energy Technologies Office (WETO), November, 29, 2018. Distributed by A2E. https://doi.org/10.21947/1483820
@misc{OEDI_Dataset_4209, title = {UAE6 - Wind Tunnel Tests Data - UAE6 - Sequence N - Raw Data}, author = {Fingersh, Lee}, abstractNote = {**Overview**

Sequence N: Sin AOA, Rotating (P)

This sequence was designed to quantify the blade 3-D unsteady aerodynamic response in the
presence of rotational influences by varying blade pitch angle. Test sequence N used an upwind,
rigid turbine with a 0° cone angle. The wind speed was 15 m/s, and the yaw angle was 0°
throughout the sequence. The rotor rotated at 72 RPM. Blade and probe pressure measurements
were collected. 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.

Sinusoidal angle-of-attack histories were designed to emulate 2-D S809 dynamic data obtained at
the Ohio State University (OSU) wind tunnel (Reuss Ramsey et al. 1995) and the 1P yawed flow
angle-of-attack variations the turbine could be expected to encounter in routine operation. The
reduced frequency (K), mean angle of attack (?m), and oscillation amplitude (??) were computed
for each of the five primary span locations. The file lengths varied according to the time required
to complete 40 oscillations at the specified frequency. The file name convention used the
sequence designation N, followed by two digits for the span location (30, 47, 63, 80, or 95),
followed by two digits representing the condition specified in the test matrix, followed by the
repetition digit. Due to time constraints, most of the test conditions corresponding to the 63\%
span location were eliminated. Test points with a
static pitch angle of 3° were collected throughout the sequence to ascertain instrumentation fidelity.

**Data Details**

File naming information can be found in the attached Word document "Sequence N Filename Key", copied from the Phase VI Test Report.}, url = {https://a2e.energy.gov/data/uae6/uae6.z13.00}, year = {2018}, howpublished = {A2E, Wind Energy Technologies Office (WETO), https://doi.org/10.21947/1483820}, note = {Accessed: 2025-05-07}, doi = {10.21947/1483820} }
https://dx.doi.org/10.21947/1483820

Details

Data from Nov 29, 2018

Last updated Mar 27, 2020

Submitted Nov 29, 2018

Organization

Wind Energy Technologies Office (WETO)

Contact

Lee Fingersh

303.384.6929

Authors

Lee Fingersh

NREL

Research Areas

DOE Project Details

Project Name Wind Data Hub

Project Number 67025

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