Abstract
A method to quantify the local inflow vector on a rotating turbine blade using a five-hole static pressure probe was developed at the National Wind Technology Center. The technique permits quantification of dynamic pressure, angle-of-attack, and cross-flow-angle to magnitudes of +/- 40 deg in any inflow direction parallel to the probe centerline. A description of the static and dynamic calibration procedure, iteration sequence for data reduction, and field results are included.
Original language | American English |
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Pages | 1-7 |
Number of pages | 7 |
State | Published - 1997 |
Event | 35th Aerospace Sciences Meeting and Exhibit, 1997 - Reno, United States Duration: 6 Jan 1997 → 9 Jan 1997 |
Conference
Conference | 35th Aerospace Sciences Meeting and Exhibit, 1997 |
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Country/Territory | United States |
City | Reno |
Period | 6/01/97 → 9/01/97 |
Bibliographical note
Publisher Copyright:© 1997 American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
NREL Publication Number
- NREL/CP-500-22134
Keywords
- tunnel calibration
- turbines
- wind
- wind