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Found 30 datasets matching filters. (clear all filters)

  • #1 Federal

    **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],...

    Search relevance: 1.00 | Views last month: 3 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #2 Federal

    **Overview** Sequences B, C, and D: Downwind Baseline (F), Downwind Low Pitch (F), Downwind High Pitch (F) This test sequence used a downwind, teetered turbine with a 3.4° cone angle. The wind...

    Search relevance: 1.00 | Views last month: 2 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #3 Federal

    **Overview** Sequence V: Tip Plate (F) This test sequence used an upwind, rigid turbine with a 0° cone angle. The wind speed ranged from 5 m/s to 25 m/s, and the yaw angle was held at 0°. The...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #4 Federal

    **Overview** Sequence W: Extended Blade (F) This test sequence used an upwind, rigid turbine with a 0° cone angle. The wind speed ranged from 5 m/s to 21 m/s, and the yaw angle was held at 0°....

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #5 Federal

    **Overview** Sequence L: Step AOA, Parked (P) This sequence was designed to quantify the 3-D blade static angle-of-attack response in the absence of rotational influences by varying the blade...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #6 Federal

    **Overview** Sequence R: Step AOA, No Probes (P) This sequence was designed to quantify the effect of the five-hole probes on the 3-D blade static angle-of-attack response in the presence of...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #7 Federal

    **Overview** Sequence G: Upwind Teetered (F) Test sequence G used an upwind, teetered turbine with a 0° cone angle. The wind speeds ranged from 5 m/s to 25 m/s. Yaw angles of ±180° were achieved...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #8 Federal

    **Overview** Sequences H, I, and J: Upwind Baseline (F), Upwind Low Pitch (F), Upwind High Pitch (F) This test sequence used an upwind, rigid turbine with a 0° cone angle. The wind speed...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #9 Federal

    **Overview** Sequences 8 and 9: Downwind Sonics (F,P) and Downwind Sonics Parked (P) This test sequence used an upwind, rigid turbine with a 0° cone angle. The wind speed ranged from 5 m/s to 25...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #10 Federal

    **Overview** Sequences B, C, and D: Downwind Baseline (F), Downwind Low Pitch (F), Downwind High Pitch (F) This test sequence used a downwind, teetered turbine with a 3.4° cone angle. The wind...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #11 Federal

    **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...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #12 Federal

    **Overview** Sequences B, C, and D: Downwind Baseline (F), Downwind Low Pitch (F), Downwind High Pitch (F) This test sequence used a downwind, teetered turbine with a 3.4° cone angle. The wind...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #13 Federal

    **Overview** Sequences S, T, and U: Upwind, No Probes (F); Upwind 2° Pitch (F); Upwind 4° Pitch (F) This test sequence used an upwind, rigid turbine with a 0° cone angle. The wind speed...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #14 Federal

    **Overview** Sequence K: Step AOA, Probes (P) This sequence was designed to quantify the 3-D blade static angle-of-attack response in the presence of rotational influences by varying the blade...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #15 Federal

    **Overview** Sequences H, I, and J: Upwind Baseline (F), Upwind Low Pitch (F), Upwind High Pitch (F) This test sequence used an upwind, rigid turbine with a 0° cone angle. The wind speed...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #16 Federal

    **Overview** Sequence O: Sin AOA, Parked (P) This sequence was designed to quantify the blade 3-D unsteady aerodynamic response in the absence of rotational influences by varying blade pitch...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #17 Federal

    **Overview** Sequences S, T, and U: Upwind, No Probes (F); Upwind 2° Pitch (F); Upwind 4° Pitch (F) This test sequence used an upwind, rigid turbine with a 0° cone angle. The wind speed...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #18 Federal

    **Overview** Sequence 3: Tower Wake Measure (P) Sequence 3 used a downwind, rigid turbine with a 3.4° cone angle. The wind speeds for this sequence corresponded to subcritical [7 m/s],...

    Search relevance: 1.00 | Views last month: 1 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #19 Federal

    **Overview** Sequence 7: Shroud Operating (P) This test sequence used a downwind, rigid turbine with a 3.4° cone angle. The wind speed ranged from 5 m/s to 25 m/s. Turntable angles from 0° to...

    Search relevance: 1.00 | Views last month: 0 | Catalog Last Checked: April 25, 2026 at 08:41 AM
  • #20 Federal

    **Overview** Sequence Q: Dynamic Inflow (P) This sequence was designed to characterize the dynamic inflow variation using the five-hole probes that extend upwind of the leading edge of the...

    Search relevance: 1.00 | Views last month: 0 | Catalog Last Checked: April 25, 2026 at 08:41 AM

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