Rotary Wing CLFC TERMINATED
Closed-Loop Flow Control to Enhance Aerodynamic and Aeroacoustic Performance of Wind-Turbine Blades
Total Cost €
0EC-Contrib. €
0Partnership
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0Rotary Wing CLFC project word cloud
Explore the words cloud of the Rotary Wing CLFC project. It provides you a very rough idea of what is the project "Rotary Wing CLFC" about.
Project "Rotary Wing CLFC" data sheet
The following table provides information about the project.
| Coordinator |
TECHNISCHE UNIVERSITAT BERLIN
Organization address contact info |
| Coordinator Country | Germany [DE] |
| Project website | http://www.forschung.tu-berlin.de/eu_buero/menue/foerderprojekte_an_der_tu_berlin/horizont_2020_msca_marie_sklodowska_curie_actions/ |
| Total cost | 171˙460 € |
| EC max contribution | 171˙460 € (100%) |
| Programme |
1. H2020-EU.1.3.2. (Nurturing excellence by means of cross-border and cross-sector mobility) |
| Code Call | H2020-MSCA-IF-2014 |
| Funding Scheme | MSCA-IF-EF-ST |
| Starting year | 2015 |
| Duration (year-month-day) | from 2015-05-01 to 2017-04-30 |
Partnership
Take a look of project's partnership.
| # | ||||
|---|---|---|---|---|
| 1 | TECHNISCHE UNIVERSITAT BERLIN | DE (BERLIN) | coordinator | 171˙460.00 |
Map
Project objective
Aerodynamic loads and noise emitted from rotating blades are of interest in many industrial applications, such as wind-turbines, aircraft propellers, helicopter blades, and cooling fans. This research project aims to achieve, for the first time, a combined aerodynamic and aeroacoustic optimization of rotary wing by experiments conducted in a controlled environment of gusting flow and rotating motion. In the current work focus will be made on wind-turbine applications. Both passive and active flow control technologies will be utilized to enhance the amount of energy harvested from the wind, while improving the aeroacoustic properties. Leading- and trailing-edge serration have proven to be effective in reducing the noise emitted from wind-turbine blades. However, their effectiveness under realistic flow conditions in a controlled environment has not been investigated. These experiments will be used for further development and validation of new aerodynamic and aeroacoustic models. The ultimate and final goal is to apply closed-loop flow control by utilizing a physics based model. Alongside these experiments, innovative and stand-alone technology for data acquisition and control in rotating blade environments will be developed and implemented. This holistic interdisciplinary approach, bringing together the aerodynamic and aeroacoustic behaviour of wind-turbine blades under realistic flow conditions into one comprehensive study is unique and novel, and will lead to major advances in our understanding of rotating blades aerodynamics and aeroacoustics.
Publications
| year | authors and title | journal | last update |
|---|---|---|---|
| 2017 |
Ben-Gida, H., Faran, M., Kogan, T. Noise reduction of a UAV propeller using grit-type boundary layer tripping published pages: , ISSN: , DOI: |
57th Israel Annual Conference on Aerospace Sciences, Tel-Aviv & Haifa, Israel, March 15-16, 2017 | 2019-06-14 |
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