Active Aerodynamic Load Control of Blades Using Small Flaps or Tabs.
Abstract
Abstract not provided.
- Authors:
- Publication Date:
- Research Org.:
- Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
- Sponsoring Org.:
- USDOE National Nuclear Security Administration (NNSA)
- OSTI Identifier:
- 1147885
- Report Number(s):
- SAND2007-2822C
523236
- DOE Contract Number:
- AC04-94AL85000
- Resource Type:
- Conference
- Resource Relation:
- Conference: Proposed for presentation at the European Wind Energy Conference & Exhibition held May 7-10, 2007 in Milan, Italy.
- Country of Publication:
- United States
- Language:
- English
Citation Formats
Zayas, Jose R. Active Aerodynamic Load Control of Blades Using Small Flaps or Tabs.. United States: N. p., 2007.
Web.
Zayas, Jose R. Active Aerodynamic Load Control of Blades Using Small Flaps or Tabs.. United States.
Zayas, Jose R. Tue .
"Active Aerodynamic Load Control of Blades Using Small Flaps or Tabs.". United States.
doi:. https://www.osti.gov/servlets/purl/1147885.
@article{osti_1147885,
title = {Active Aerodynamic Load Control of Blades Using Small Flaps or Tabs.},
author = {Zayas, Jose R.},
abstractNote = {Abstract not provided.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue May 01 00:00:00 EDT 2007},
month = {Tue May 01 00:00:00 EDT 2007}
}
Other availability
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System ID modern control algorithms for active aerodynamic load control and impact on gearbox loading.
Prior work on active aerodynamic load control (AALC) of wind turbine blades has demonstrated that appropriate use of this technology has the potential to yield significant reductions in blade loads, leading to a decrease in wind cost of energy. While the general concept of AALC is usually discussed in the context of multiple sensors and active control devices (such as flaps) distributed over the length of the blade, most work to date has been limited to consideration of a single control device per blade with very basic Proportional Derivative controllers, due to limitations in the aeroservoelastic codes used to performmore »