DOE PAGES title logo U.S. Department of Energy
Office of Scientific and Technical Information

Title: Modeling dynamic stall on wind turbine blades under rotationally augmented flow fields

Abstract

Abstract This paper presents an investigation of two well‐known aerodynamic phenomena, rotational augmentation and dynamic stall, together in the inboard parts of wind turbine blades. This analysis is carried out using the following: (1) the National Renewable Energy Laboratory's Unsteady Aerodynamics Experiment Phase VI experimental data, including constant as well as continuously pitching blade conditions during axial operation; (2) data from unsteady delayed detached eddy simulations (DDES) carried out using the Technical University of Denmark's in‐house flow solver Ellipsys3D; and (3) data from a reduced order dynamic stall model that uses rotationally augmented steady‐state polars obtained from steady Phase VI experimental sequences, instead of the traditional two‐dimensional, non‐rotating data. The aim of this work is twofold. First, the blade loads estimated by the DDES simulations are compared with three select cases of the N‐sequence experimental data, which serves as a validation of the DDES method. Results show reasonable agreement between the two data in two out of three cases studied. Second, the dynamic time series of the lift and the moment polars obtained from the experiments are compared with those from the dynamic stall model. This allowed the differences between the stall phenomenon on the inboard parts of harmonically pitchingmore » blades on a rotating wind turbine and the classic dynamic stall representation in two‐dimensional flow to be investigated. Results indicated a good qualitative agreement between the model and the experimental data in many cases, which suggests that the current two‐dimensional dynamic stall model as used in blade element momentum‐based aeroelastic codes may provide a reasonably accurate representation of three‐dimensional rotor aerodynamics when used in combination with a robust rotational augmentation model. Copyright © 2015 John Wiley & Sons, Ltd.« less

Authors:
 [1];  [2];  [1]; ORCiD logo [2]
  1. National Renewable Energy Laboratory 15013 Denver West Parkway Golden CO 80401 USA
  2. Department of Wind Energy Technical University of Denmark ‐ Risø campus Roskilde 4000 Denmark
Publication Date:
Sponsoring Org.:
USDOE
OSTI Identifier:
1401379
Resource Type:
Publisher's Accepted Manuscript
Journal Name:
Wind Energy
Additional Journal Information:
Journal Name: Wind Energy Journal Volume: 19 Journal Issue: 3; Journal ID: ISSN 1095-4244
Publisher:
Wiley Blackwell (John Wiley & Sons)
Country of Publication:
United Kingdom
Language:
English

Citation Formats

Guntur, Srinivas, Sørensen, Niels N., Schreck, Scott, and Bergami, Leonardo. Modeling dynamic stall on wind turbine blades under rotationally augmented flow fields. United Kingdom: N. p., 2015. Web. doi:10.1002/we.1839.
Guntur, Srinivas, Sørensen, Niels N., Schreck, Scott, & Bergami, Leonardo. Modeling dynamic stall on wind turbine blades under rotationally augmented flow fields. United Kingdom. https://doi.org/10.1002/we.1839
Guntur, Srinivas, Sørensen, Niels N., Schreck, Scott, and Bergami, Leonardo. Mon . "Modeling dynamic stall on wind turbine blades under rotationally augmented flow fields". United Kingdom. https://doi.org/10.1002/we.1839.
@article{osti_1401379,
title = {Modeling dynamic stall on wind turbine blades under rotationally augmented flow fields},
author = {Guntur, Srinivas and Sørensen, Niels N. and Schreck, Scott and Bergami, Leonardo},
abstractNote = {Abstract This paper presents an investigation of two well‐known aerodynamic phenomena, rotational augmentation and dynamic stall, together in the inboard parts of wind turbine blades. This analysis is carried out using the following: (1) the National Renewable Energy Laboratory's Unsteady Aerodynamics Experiment Phase VI experimental data, including constant as well as continuously pitching blade conditions during axial operation; (2) data from unsteady delayed detached eddy simulations (DDES) carried out using the Technical University of Denmark's in‐house flow solver Ellipsys3D; and (3) data from a reduced order dynamic stall model that uses rotationally augmented steady‐state polars obtained from steady Phase VI experimental sequences, instead of the traditional two‐dimensional, non‐rotating data. The aim of this work is twofold. First, the blade loads estimated by the DDES simulations are compared with three select cases of the N‐sequence experimental data, which serves as a validation of the DDES method. Results show reasonable agreement between the two data in two out of three cases studied. Second, the dynamic time series of the lift and the moment polars obtained from the experiments are compared with those from the dynamic stall model. This allowed the differences between the stall phenomenon on the inboard parts of harmonically pitching blades on a rotating wind turbine and the classic dynamic stall representation in two‐dimensional flow to be investigated. Results indicated a good qualitative agreement between the model and the experimental data in many cases, which suggests that the current two‐dimensional dynamic stall model as used in blade element momentum‐based aeroelastic codes may provide a reasonably accurate representation of three‐dimensional rotor aerodynamics when used in combination with a robust rotational augmentation model. Copyright © 2015 John Wiley & Sons, Ltd.},
doi = {10.1002/we.1839},
journal = {Wind Energy},
number = 3,
volume = 19,
place = {United Kingdom},
year = {Mon Mar 09 00:00:00 EDT 2015},
month = {Mon Mar 09 00:00:00 EDT 2015}
}

Journal Article:
Free Publicly Available Full Text
Publisher's Version of Record
https://doi.org/10.1002/we.1839

Citation Metrics:
Cited by: 21 works
Citation information provided by
Web of Science

Save / Share:

Works referenced in this record:

Fluid mechanics of dynamic stall part II. Prediction of full scale characteristics
journal, March 1988


Blade Dynamic Stall Vortex Kinematics for a Horizontal Axis Wind Turbine in Yawed Conditions*
journal, June 2001

  • Schreck, Scott J.; Robinson, Michael C.; Hand, M. Maureen
  • Journal of Solar Energy Engineering, Vol. 123, Issue 4
  • DOI: 10.1115/1.1408307

Low Frequency Shedding Prompted by Three-Dimensionality Under Rotational Augmentation
conference, June 2010

  • Schreck, Scott
  • 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
  • DOI: 10.2514/6.2010-640

On the formation and control of the dynamic stall vortex on a pitching airfoil
conference, August 1991


On the birth of stall cells on airfoils
journal, March 2010

  • Rodríguez, Daniel; Theofilis, Vassilis
  • Theoretical and Computational Fluid Dynamics, Vol. 25, Issue 1-4
  • DOI: 10.1007/s00162-010-0193-7

Geometric Conservation Law and Its Application to Flow Computations on Moving Grids
journal, October 1979

  • Thomas, P. D.; Lombard, C. K.
  • AIAA Journal, Vol. 17, Issue 10
  • DOI: 10.2514/3.61273

Fluid mechanics of dynamic stall part I. Unsteady flow concepts
journal, January 1988


An evaluation of several methods of determining the local angle of attack on wind turbine blades
journal, December 2014


Dynamic Stall on Rotating Airfoils: A Look at the N-Sequence Data from the NREL Phase VI Experiment
journal, July 2013


Zonal Two Equation k-w Turbulence Models For Aerodynamic Flows
conference, February 2013

  • Menter, F.
  • 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference
  • DOI: 10.2514/6.1993-2906

Delaying Effect of Rotation on Laminar Separation
journal, April 1963

  • Banks, W. H. H.; Gadd, G. E.
  • AIAA Journal, Vol. 1, Issue 4
  • DOI: 10.2514/3.1687

A study on rotational effects and different stall delay models using a prescribed wake vortex scheme and NREL phase VI experiment data
journal, September 2008

  • Breton, Simon-Philippe; Coton, Frank N.; Moe, Geir
  • Wind Energy, Vol. 11, Issue 5
  • DOI: 10.1002/we.269

Dynamic Stall and Aerodynamic Damping
journal, August 1999

  • Rasmussen, F.; Petersen, J. T.; Madsen, H. A.
  • Journal of Solar Energy Engineering, Vol. 121, Issue 3
  • DOI: 10.1115/1.2888426

Predicting 2D Airfoil and 3D Wind Turbine Rotor Performance using a Transition Model for General CFD Codes
conference, June 2006

  • Langtry, Robin; Gola, Janusz; Menter, Florian
  • 44th AIAA Aerospace Sciences Meeting and Exhibit
  • DOI: 10.2514/6.2006-395

Comparing different dynamic stall models: Comparing different dynamic stall models
journal, April 2012

  • Holierhoek, J. G.;  de Vaal, J. B.;   van Zuijlen, A. H.
  • Wind Energy, Vol. 16, Issue 1
  • DOI: 10.1002/we.548

A Correlation-Based Transition Model Using Local Variables: Part I — Model Formulation
conference, November 2008

  • Menter, F. R.; Langtry, R. B.; Likki, S. R.
  • ASME Turbo Expo 2004: Power for Land, Sea, and Air, Volume 4: Turbo Expo 2004
  • DOI: 10.1115/GT2004-53452

Rotational augmentation of horizontal axis wind turbine blade aerodynamic response
journal, January 2002

  • Schreck, S.; Robinson, M.
  • Wind Energy, Vol. 5, Issue 2-3
  • DOI: 10.1002/we.68

Detached eddy simulation of massively separated flows
conference, February 2013


Insight into Rotational Effects on a Wind Turbine Blade Using Navier–Stokes Computations
journal, October 2014

  • Herráez, Iván; Stoevesandt, Bernhard; Peinke, Joachim
  • Energies, Vol. 7, Issue 10
  • DOI: 10.3390/en7106798

Transitional DDES computations of the NREL Phase-VI rotor in axial flow conditions
journal, December 2014


Influence of Rotation on Dynamic Stall
journal, July 2013

  • Gardner, A. D.; Richter, K.
  • Journal of the American Helicopter Society, Vol. 58, Issue 3
  • DOI: 10.4050/JAHS.58.032001

Progress in analysis and prediction of dynamic stall
journal, January 1988

  • Carr, Lawrence W.
  • Journal of Aircraft, Vol. 25, Issue 1
  • DOI: 10.2514/3.45534

Lift-curve characteristics for an airfoil pitching at constant rate
conference, August 1986


A Semi-Empirical Model for Dynamic Stall
journal, July 1989

  • Leishman, J. G.; Beddoes, T. S.
  • Journal of the American Helicopter Society, Vol. 34, Issue 3
  • DOI: 10.4050/JAHS.34.3