Estimating the Unsteady Angle of Attack from Blade Pressure Measurments on the NREL Phase VI Rotor in Yaw using a Free-Wake Vortex Model

Estimating the Unsteady Angle of Attack from Blade Pressure Measurments on the NREL Phase VI Rotor in Yaw using a Free-Wake Vortex Model

Author(s):

T. Sant ( Delft University of Technology, Delft, The Netherlands )
G. van Kuik
G. van Bussel

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2006

Pub. Year:

2006

No.:

2006-0393

Paper no.:

AIAA Paper 2006-393

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200602 [CD-ROM 2006 Disc 2]

Type:

Technical Paper

Details

TDL ID:	ZA00047217
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	44th
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2006.01.09-2009.01.12

Similar Items:

1 Technical Paper Measurement and Modelling of Tip Vortex Paths in the Wake of a HAWT Under Yawed Flow Conditions Haans, W., Sant, T., van Kuik, G., van Bussel, G. American Institute of Aeronautics and Astronautics	7 Technical Paper Transient Rotor Inflow Using a Time-Accurate Free-Vortex Wake Model Bhagwat,Mahendra J., Leishman,J.Gordon American Institute of Aeronautics and Astronautics
2 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	8 Technical Paper Prediction of unsteady rotor-surface pressure and heat transfer from wake passings Tran, Le T., Taulbee, Dale B. The American Society of Mechanical Engineers
3 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	9 Technical Paper PIV Visualization of Dynamic Stall VAWT and Blade Load Determination C. Simao Ferreira, G. van Bussel, F. Scarano, G. van Kuik American Institute of Aeronautics and Astronautics
4 Technical Paper Performance Predictions Of NREL Phase VI Combined Experiment Rotor Using A Free-Vortex Wake Model S. Gupta, J. Leishman American Institute of Aeronautics and Astronautics	10 Technical Paper Validation Of A Free-Vortex Wake Model For Wind Turbines In Yawed Flow S. Gupta, J. Leishman American Institute of Aeronautics and Astronautics
5 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	11 Technical Paper PREDICTION OF UNSTEADY BLADE SURFACE PRESSURES ON AN ADVANCED PROPELLER AT AN ANGLE OF ATTACK Nallasamy, M., Groeneweg, J. F. National Aeronautics and Space Adminstration
6 Technical Paper Time-Accurate Modeling of Rotor Wakes using a Free-Vortex Wake Method Bhagwat,M., Leishman,J. American Institute of Aeronautics and Astronautics	12 Technical Paper Unsteady Aerodynamic Modeling at High Angles of Attack Tianfeng,J., Zhenghong,G. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12