PIV Visualization of Dynamic Stall VAWT and Blade Load Determination

PIV Visualization of Dynamic Stall VAWT and Blade Load Determination

Author(s):

C. Simao Ferreira ( Delft University of Technology, Delft, The Netherlands )
G. van Bussel
F. Scarano
G. van Kuik

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-1317

Paper no.:

AIAA Paper 2008-1317

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200801 [CD-ROM 2008 Disc 1]

Type:

Technical Paper

Details

TDL ID:	ZA00049519
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	46th
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2008.01.07-2008.01.10
Note for article:	46th AIAA Aerospace Sciences Meeting and Exhibit, 7-10 January 2008, Reno, Nevada

Similar Items:

1 Technical Paper 2D PIV Visualization of Dynamic Stall on a Vertical Axis Wind Turbine C. Simao Ferreira, G. Van Bussel, G. Van Kuik, F. Scarano American Institute of Aeronautics and Astronautics	7 Technical Paper Closed-Loop Control Wind Tunnel Tests on an Adaptive Wind Turbine Blade for Load Reduction T. Barlas, J. van Wingerden, A. Hulskamp, G. van Kuik American Institute of Aeronautics and Astronautics
2 Technical Paper 2D CFD Simulation of Dynamic Stall on a Vertical Axis Wind Turbine: Verification and Validation with PIV Measurements C. Simao Ferreira, G. van Bussel, G. Van Kuik American Institute of Aeronautics and Astronautics	8 Technical Paper Vortex Wake Investigation of an Airbus A340 Model Using PIV in a Towing Tank Veldhuis, L., Scarano, F., Wijk, C. American Institute of Aeronautics and Astronautics
3 Technical Paper Wind tunnel hotwire measurements, flow visualization and thrust measurement of a VAWT in skew C. Ferreira, G. van Kuik, G. van Bussel American Institute of Aeronautics and Astronautics	9 Technical Paper Performance of a High Tip Speed Ratio H-Darrieus in the Skewed Flow on a Roof Mertens, S., Kuik, G., Bussel, G. American Institute of Aeronautics and Astronautics
4 Technical Paper The VAWT in Skew: Stereo-PIV and Vortex Modeling C. Ferreira, K. Dixon, C. Hofemann, G. van Kuik, G. van Bussel American Institute of Aeronautics and Astronautics	10 Technical Paper The Inverse Vortex Wake Model: A Measurement Analysis Tool W. Haans, G. van Kuik, G. van Bussel American Institute of Aeronautics and Astronautics
5 Technical Paper Stall in Yawed Flow Conditions: a Correlation of Blade Element Momentum Predictions with Experiments W. Haans, G. van Bussel, T. Sant, G. van Kuik American Institute of Aeronautics and Astronautics	11 Technical Paper Particle Image Velocimetry Based Loads Determination in Supersonic Flows L. Souverein, B. van Oudheusden, F. Scarano American Institute of Aeronautics and Astronautics
6 Technical Paper Estimating the Unsteady Angle of Attack from Blade Pressure Measurments on the NREL Phase VI Rotor in Yaw using a Free-Wake Vortex Model T. Sant, G. van Kuik, G. van Bussel American Institute of Aeronautics and Astronautics	12 Technical Paper The Edge Singularity of an Actuator Disc with a Constant Normal Load Kuik, G. van American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12