[en] A solver has been developed within the OpenFoam framework to compute large amplitude
motion of two-dimensional rigid configurations. The results obtained with this code
were successfully validated on rigid airfoils at static and dynamic conditions, as well as
correlated with experimental data and numerical solutions from similar unsteady solvers.
The results demonstrated that while current computational methods are able to predict the
self-sustained oscillations characterizing a pitch-dominated stall flutter, including energy
transfer, improvements are needed. The influence of grid, temporal integration, turbulence
modeling, and flow equations is examined for the stall flutter starting solution of dynamic
stall.
Disciplines :
Ingénierie aérospatiale
Auteur, co-auteur :
Watrin, Damien ; Université de Liège - ULiège > Département d'aérospatiale et mécanique > Interactions Fluide-Structure - Aérodynamique expérimentale
Dimitriadis, Grigorios ; Université de Liège - ULiège > Département d'aérospatiale et mécanique > Interactions Fluide-Structure - Aérodynamique expérimentale
Perry, Tristan; Georgia Institute of Technology > School of Aerospace Engineering
Smith, Marilyn J.; Georgia Institute of Technology > School of Aerospace Engineering
Langue du document :
Anglais
Titre :
Computational Considerations for the Prediction of Stall Flutter
Date de publication/diffusion :
25 avril 2012
Nom de la manifestation :
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Organisateur de la manifestation :
American Institute of Aeronautics and Astronautics
Lieu de la manifestation :
Honolulu, Hawaii, Etats-Unis
Date de la manifestation :
from 23-04-2012 to 26-04-2012
Manifestation à portée :
International
Titre de l'ouvrage principal :
Proceedings of the 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Ham, N. D. and Young, M. I., "Limit Cycle Torsional Motion of Helicopter Blades due to Stall, " Journal of Sound and Vibration, Vol. 4, No. 3, 1966, pp. 431-432.
Ericsson, L. E., "Role of Stall Flutter in the Double-Stall Phenomenon of Wind-Turbine Blades, " Journal of Aircraft, Vol. 37, No. 1, 2000, pp. 104-109.
Holierhoek, J. G., "Investigation into the possibility of flap-lag-stall flutter, " 45th AIAA Aerospace Sciences Meeting and Exhibit, No. AIAA 2007-211, Reno, Nevada, Jan. 2007.
Victory, M., "Flutter at high incidence, " Reports and Memoranda No. 2048, Aeronautical Research Committee, 1943.
Rivera, Jr., J. A., Dansburry, B. E., Bennett, R. M., Durham, M. H., and Silva, W. A., "NACA 0012 benchamrk model experimental flutter results with unsteady pressure distributions, " Proceedings of the 33rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, No. AIAA 1992-2396, Dallas, Texas, April 1992.
Poirel, D., Harris, Y., and Benaissa, A., "Self-sustained aeroelastic oscillations of a NACA 0012 airfoil at low-to-moderate Reynolds numbers, " Journal of Fluids and Structures, Vol. 24, No. 5, 2008, pp. 700719.
Poirel, D. and Yuan, W., "Aerodynamics of laminar separation flutter at a transitional Reynolds number, " Journal of Fluids and Structures, Vol. 26, No. 7-8, 2010, pp. 1174-1194.
Poirel, D. and Mendes, F., "Experimental Investigation of Small Amplitude Self-Sustained Pitch-Heave Oscillations of a NACA0012 Airfoil at Transitional Reynolds Numbers, " 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, No. AIAA 2012-0040, Nashville, Tennessee, Jan. 2012.
Dimitriadis, G. and Li, J., "Bifurcation Behavior of Airfoil Undergoing Stall Flutter Oscillations in Low-Speed Wind Tunnel, " AIAA Journal, Vol. 47, No. 11, 2009, pp. 2577-2596.
Razak, N. and Dimitriadis, G., "Flutter and Stall Flutter of a Rectangular Wing in a Wind Tunnel, " AIAA Journal, Vol. 49, No. 10, 2011, pp. 2258-2271.
Razak, N., Rothkegel, J. I., and Dimitriadis, G., "Wind tunnel experiments on a pitch-plunge wing undergoing limit cycle oscillation, " 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Honolulu, Hawaii, April 2012.
Smith, M., Wong, T., Potsdam, M., Baeder, J., and Phanse, S., "Evaluation of CFD to Determine Two-Dimensional Airfoil Characteristics for Rotorcraft Applications, " Journal of the American Helicopter Society, Vol. 50, No. 1, 2006, pp. 70-79.
Smith, M. J., Liggett, N. D., and Koukol, B. C. G., "Aerodynamics of Airfoils at High and Reverse Angles of Attack, " Journal of Aircraft, Vol. 48, No. 6, 2011, pp. 2012-2023.
Liggett, N. and Smith, M., "Temporal Convergence Criteria for Time-Accurate Viscous Simulations of Separated Flows, " Under revision for the Journal of Computers and Fluids, 2011.
Sanchez-Rocha, M., Kirtas, M., and Menon, S., "Zonal Hybrid RANS-LES Method for Static and Oscillating Airfoils and Wings, " 44th AIAA Aerospace Sciences Meeting, AIAA 2006-1256, Reno, NV, January 2006.
Sanchez-Rocha, M., Wall-Models for Large Eddy Simulation Based on a Generic Additive-Filter Formulation, Ph. D. thesis, Georgia Institute of Technology, December 2008.
Gleize, V. and Szydlowski, J. and Costes, M., "Numerical and Physical Analysis of the Turbulent Viscous Flow Around a NACA0015 Profile at Stall, " European Congress on Computational Methods in Applied Sciences and Engineering, Jyvaskyla, Finland, 2004.
Szydlowski, J. and Costes, M., "Simulation of flow around NACA 0015 airfoil for static and dynamic stall configurations using RANS and DES, " Tiré à part-Office national d'études et de recherches aerospatiales.
Richter, K., Le Pape, A., Knopp, T., Costes, M., Gleize, V., and Gardner, A., "Improved Two-Dimensional Dynamic Stall Prediction with Structured and Hybrid Numerical Methods, " Journal of the American Helicopter Society, Vol. 56, No. 4, 2011, pp. 1-12.
Moulton, M. and Smith, M. J., "The Prediction and Validation of Static and Dynamic Stall, " Proceedings of the AHS International Meeting on Advanced Rotorcraft Technology and Safety Operations, Ohmiya, Japan, November 1-3 2010.
Gleize, V., Le Pape, A., Costes, M., and Richez, F., "Numerical simulation of a pitching airfoil under dynamic stall conditions including laminar/turbulent transition, " AIAA paper 2008-0391, 2008, 46thAerospace SciencesMeeting andExhibit, Reno, NV, January 7-10.
Moulton, M., Smith, M. J., Wong, T.-C., Pape, A. L., and Balleur, J.-C. L., "The Role of Transition Modeling in CFD Predictions of Static and Dynamic Stall, " Proceedings of the 37th European Rotorcraft Forum, Gallarate, Italy, Sept. 2011.
Medida, S. and Baeder, J., "Application of the Correlation-based Gamma-Re Theta t Transition Model to the Spalart-Allmaras Turbulence Model, " AIAA-2011-3979, 2011, 20th AIAA Computational Fluid Dynamics Conference, Honolulu, HI, June 27-30.
Medida, S. and Baeder, J., "Numerical Investigation of 3-D Dynamic Stall using Delayed Detached Eddy Simulation, " AIAA-2012-099, 2012, 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Nashville, Tennessee, Jan. 9-12.
Yabili, S., Development and Validation of a Solver for the Prediction of Low-Reynolds Dynamic Stall and Stall Flutter, Master's thesis, University of Liège, Belgium, September 2011.
Yabili, S., Smith, M. J., and Dimitriadis, G., "Unsteady Navier-Stokes Simulation of Low-Reynolds Stall Flutter, " AIAA 50th Aerospace Sciences Meeting and Exhibit, No. AIAA-2012-TBD, Nashville, Tennessee, January 9-12 2012.
Li, J., Experimental Investigation of the Low Speed Stall Flutter of an Airfoil, Ph. D. thesis, University of Manchester, UK, 2009.
Wang, B., Poirel, D., Yuan, W., and Zha, G.-C., "Numerical Simulation of Self-sustained Oscillations of an Airfoil at a Transitional Reynolds Number using High-order Schemes, " 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, No. AIAA 2011-2139, Denver, Colorado, April 2011.
McCroskey, W. J., McAlister, K. W., Carr, L. W., and Pucci, S. L., "An Experimental Study of Dynamic Stall on Advanced Airfoil Sections, " Technical Memorandum 84245, NASA, 1982.
Ferziger, J. H. and Peric, M., Computational Methods for Fluid Dynamics, Spinger, 3rd Ed., 1996.
Menter, F., "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications, " AIAA Journal, Vol. 32, No. 8, August 1994, pp. 1598-1605.
Jasak, H. and Tuković, Z., "Dynamic Mesh Handling in OpenFoam Applied to Fluid-Structure Interaction Simulation, " Proceedings of the 5th European Conference on Computational Fluid Dynamics, ECCOMAS CFD 2010, Lisbon, Portugal, June 2010.
Chan, W., Meakin, R., and Potsdam, M., "CHSSI Software for Geometrically Complex Unsteady Aerodynamic Applications, " 15th AIAA Computational Fluid Dynamics Conference, No. AIAA-2001-0593, Anaheim, CA, June 11-14 2001.
Harris, C., "Two Dimensional Aerodynamic Characteristics of the NACA 0012 Airfoil in the Langley 8-foot Transonic Pressure Tunnel, " Technical Memorandum 81917, NASA, 1981.
Geuzaine, C. and Remacle, J.-F., "Gmsh: a three-dimensional finite element mesh generator with built-in pre-and post-processing facilities, " International Journal for Numerical Methods in Engineering, Vol. 79, 2009, pp. 1039-1331.
Abbott, I. and Doenhoff, A. V., Theory of wing sections including a summary of airfoil data, Dover Publications, Inc., 2nd ed., 1959.
Lee, T. and Gerontakos, P., "Investigation of Flow Over an Oscillating Airfoil, " Journal of Fluid Mechanics, Vol. 512, 2004, pp. 313-341.
