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Development and testing of tip devices for horizontal axis wind turbinesA theoretical and field experimental program has been carried out to investigate the use of tip devices on horizontal axis wind turbine rotors. The objective was to improve performance by the reduction of tip losses. While power output can always be increased by a simple radial tip extension, such a modification also results in an increased gale load both because of the extra projected area and longer moment arm. Tip devices have the potential to increase power output without such a structural penalty. A vortex lattice computer model was used to optimize three basic tip configuration types for a 25 kW stall limited commercial wind turbine. The types were a change in tip planform, and a single-element and double-element nonplanar tip extension (winglets). A complete data acquisition system was developed which recorded three wind speed components, ambient pressure, temperature, and turbine output. The system operated unattended and could perform real-time processing of the data, displaying the measured power curve as data accumulated in either a bin sort mode or polynomial curve fit. Approximately 270 hr of perormance data were collected over a three-month period. The sampling interval was 2.4 sec; thrus over 400,000 raw data points were logged. Results for each of the three new tip devices, compared with the original tip, showed a small decrease (of the order of 1 kW) in power output over the measured range of wind speeds from cut-in at about 4 m/s to over 20 m/s, well into the stall limiting region. Changes in orientation and angle-of-attack of the winglets were not made. For aircraft wing tip devices, favorable tip shapes have been reported and it is likely that the tip devices tested in this program did not improve rotor performance because they were not optimally adjusted.
Document ID
19860009304
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gyatt, G. W.
(AeroVironment, Inc. Monrovia, CA, United States)
Lissaman, P. B. S.
(AeroVironment, Inc. Monrovia, CA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1985
Subject Category
Energy Production And Conversion
Report/Patent Number
NAS 1.26:174991
AV-FR-85/802
NASA-CR-174991
DOE/NASA/0341-1
Report Number: NAS 1.26:174991
Report Number: AV-FR-85/802
Report Number: NASA-CR-174991
Report Number: DOE/NASA/0341-1
Accession Number
86N18774
Funding Number(s)
CONTRACT_GRANT: DEN3-341
CONTRACT_GRANT: DE-AI01-76ET-20320
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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