Prediction and physical analysis of unsteady flows around a pitching airfoil with the dynamic mesh approah

European Journal of Computational Mechanics

Volumn 16, Issue 3-4, 2007, Pages 451-476

  Bourdet, Sébastien ^a   Braza, Marianna ^a   Hoarau, Yannick ^b   El Akoury, Rajah ^a   Ashraf, Arif ^a   Harran, Gilles ^a   Chassaing, Patrick ^a   Djeridi, Henda ^c  

^a IMFT   (France)

^b Faculté de Médecine   (France)

^c French Naval Academy   (France)

Author keywords

Airfoil; Fluid structure interaction; Pitching

Indexed keywords

FLUID STRUCTURE INTERACTION; MESH GENERATION; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; VISCOUS FLOW; VORTEX FLOW;

DYNAMIC MESH; DYNAMIC MESH METHOD; FLUID-STRUCTURE INTERACTION; HIGH REYNOLDS NUMBER; MODERATE REYNOLDS NUMBERS; NAVIER-STOKES EQUATION; PHYSICAL ANALYSIS; PITCHING; PITCHING AIRFOILS; PITCHING MOTION;

AIRFOILS;

EID: 56949094177     PISSN: 26422085     EISSN: 26422050     Source Type: Journal    
DOI: 10.3166/REMN.16.451-476     Document Type: Article

References (43)

1. Ahmed S., Chandrasekhara M., « Reattachment studies of an oscillating airfoil dynamic stall flowfield », AIAA J., vol. 32, no 5, p. 1006-1012, 1994.
2. Aubrun S., « Etude expérimentale des structures cohérentes dans un écoulement turbulent décollé et comparaison avec une couche de mélange », Thèse de Doctorat, Institut National Polytechnique de Toulouse, France, 1998.
3. Barakos J., Drikakis G. A., « An implicit unfactored method for unsteady turbulent compressible flow with moving boundaries », Comp. Fluids, vol. 28, p. 899-922, 1999.
4. Batina J., « Unsteady Euler airfoil solutions using unstructured dynamic meshes », AIAA J., vol. 28, no 8, p. 1381-1388, august, 1990.
5. Blaschak J., Kriegsmann G. A., « A comparative study of absorbing boundary conditions », J. Comp. Phys., vol. 77, p. 79-130, 1988.
6. Bouhadji A., Analyse physique par simulation numérique de phénomènes de transition Bi et Tridimensionnels dans l'écoulement compressible, visqueux autour d'une aile d'avion, Thèse de doctorat, Institut National Polytechnique de Toulouse, 1998.
7. Bouhadji A., Bourdet S., Braza M., Hoarau Y., Rodes P., G.Tzabiras, « Turbulence Modelling of Unsteady Flows with a Pronounced Periodic Character », Notes on Numerical Fluid Mechanics, vol. 81, p. 87-96, 2002.
8. Bouhadji A., Braza M., « Compressibility effect on the 2D and 3D vortex structures in a transonic flow around a wing », ERCOFTAC bulletin, vol. 34, p. 4-9, 1997.
9. Bouhadji A., Braza M., « Physical analysis of unsteady viscous flow phenomena around a wing by Direct Navier-Stokes Simulation », 4th ECCOMAS Computational Fluid Dynamics Conference, Athens, 1998.
10. Bouhadji A., Braza M., « Organised modes and shock-vortex interaction in unsteady viscous transonic flows around an aerofoil. Part II:Reynolds number effect », J. Computers and Fluids, vol. 32, no 9, p. 1261-1281, 2003a.
11. Bouhadji A., Braza M., « Physical analysis by numerical simulation of organised modes and shock-vortex interaction in transonic flows around an aerofoil. Part I:Mach number effect », J. Computers and Fluids, vol. 32, no 9, p. 1233-1260, 2003b.
12. Bourdet S., Analyse physique d'écoulements compressibles instationnaires autour de structures portantes dans le contexte d'interaction fluide-structure, Thèse de doctorat, Institut National Polytechnique de Toulouse, 2005.
13. Bradshaw P., Atwell N., Ferris D., « Calculation of boundary layer development using the turbulent energy equation », J. of Fluid Mech., vol. 28, p. 593-616, 1967.
14. BrazaM., « Flow Physics Modelling in Fluid-Structure Interaction », Notes on Numerical Fluid Mechanics, dedicated volume "Progress in Computational Flow-Structure Interaction ", Sci. Eds. W. Haase, V. Selmin, B. Winzell, Publisher Springer, vol. 81, p. 145-154, 2002.
15. Braza M., Perrin R., Hoarau Y., « Turbulence Properties in the cylinder wake at high Reynolds number », J. Fluids. Struct., vol. in print, p. 1-16, 2006.
16. Carr L., McAlister K., McCroskey W., Analysis of the developpment of dynamic stall base on oscillating airfoils experiments, Technical Notes no TN-D-8382, NASA, 1977.
17. Chandrasekhara M., Carr L., « Flow visualisations studies of the Mach number effets on dynamic stall », J. Aircraft, vol. 27, p. 516-522, 1990.
18. Chien K., « Predictions of channel and boundary-layer flows with a low-Reynolds number turbulence model », AIAA Journal, vol. 20, p. 33-38, 1982.
19. Choudhuri G., Knight D., « Effects of compressibility, pitch rate, and Reynolds number on unsteady incipient leading-edge boundary layer separation over a pitching airfoil », J. Fluid Mech., vol. 308, p. 195-217, 1996.
20. Daly B., Harlow F., « Transport equations in turbulence », Physics of Fluid, vol. 13, p. 2634-2649, 1970.
21. Dervieux A., Braza M., Dussauge J., « Computation and comparison of efficient turbulence models in aeronautics », Notes on Numerical Fluid Mechanics, vol. 65, Vieweg, 1998.
22. Djeridi H., Braza M., Perrin R., Harran G., Cid E., Cazin S., « Near-Wake Turbulence Properties Around a Circular Cylinder at High Reynolds Number », J. Flow Turbulence and Combustion, vol. 71, p. 19-34, 2003.
23. Farhat C., Degand C., Koobus B., LesoinneM., « Torsional springs for two-dimensional dynamics unstructured fluid meshes », Comput. Methods Appl.Mech. Engrg., vol. 163, p. 231-245, 1998.
24. Favier D., Maresca C., Berton E., Allain C., « Etude Expérimentale et Numérique Du Développement de la Couche Limite Instationnaire sur Modèles Oscillants En Écoulements 2D/3D », D.R.E.T., Convention no 95-052, Rapport final de synthèse, Mai, 1998.
25. Guo W., Fu D., Ma Y., « Numerical investigation of dynamic stall of an oscillating airfoil », Int. J. Numer. Methods Fluids, vol. 10, p. 723-734, 1994.
26. Haase W., Selmin V., Winzell B., « Progress in Computational Flow-Structure Interaction, Results of the Project UNSI, Supported by the European Union 1998-2000 », Notes on Num. Fluid Mech. and Multidisciplinary Design, 2002.
27. Hoarau Y., Braza M., Ventikos Y., Faghani D., Tzabiras G., « Organized modes and the three-dimensional transition to turbulence in the incompressible flow around a NACA0012 wing », J. Fluid Mech., vol. 496, p. 63-72, 2003.
28. Hoarau Y., Favier D., Braza M., P.Rodes, G.Tzabiras, Allain C., Berton E., Maresca C., « Turbulence Modelling of Unsteady Flows with a Pronounced Periodic Character », IUTAM Symposium on Unsteady Separated Flows, 8-12 April 2002, Toulouse, France, 2002.
29. Jin G., Braza M., « A non-reflecting outlet boundary condition for incompressible unsteady Navier-Stokes calculations », J. Comp. Phys., vol. 107, p. 239-253, 1993.
30. Jin G., Braza M., « A Two-equation turbulence model for unsteady separated flows around airfoils », AIAA Journal, vol. 32, p. 2316-2320, 1994.
31. Launder B., Reece G., Rodi W., « Progress in the development of a Reynolds-stress turbulence closure », J. of Fluid Mech., vol. 68, p. 537-566, 1975.
32. Lefrançois E., Modèle numérique de couplage fluide-structure pour l'étude des phénomène aéroélastiques avec applications aux moteurs fusée, Thèse de doctorat, Université de Rouen, 1998.
33. McAlister K., Carr L., McCroskey W., Dynamic stall experiments on the NACA0012 airfoil, Technical Paper no TP 1100, NASA, 1978.
34. McCroskey W., « Unsteady airfoils », Ann. Rev. Fluid. Mech., vol. 14, p. 285-311, 1982.
35. McCroskey W., Carr L., McAlister K., « Dynamic stall experiments on oscillating airfoils », AIAA J., vol. 14, p. 57-63, 1976.
36. Menter F., « Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications », AIAA Journal, vol. 32, no 8, p. 1598-1605, 1994.
37. Metha U., Dynamic stall of an oscillating airfoil, Report no CP-227, AGARD, 1977.
38. Roe P., « Approximate Riemann solvers, parameter vectors and difference schemes », J. Comp. Phys., vol. 43, p. 357-372, 1981.
39. Shima N., « A Reynolds-stress model for near-wall and low-Reynolds-number regions », J. of Fluids Engng, vol. 110, p. 38-44, 1988.
40. Shu C., Osher S., « Efficient implementation of essentially non-oscillatory shock-capturing schemes », J. Comp. Phys., vol. 77, p. 439-471, 1988.
41. Thomas P., Lombard C., « Geometric conservation law and its application to flow computations on moving grids », AIAA J., vol. 17, no 10, p. 1030-1037, 1979.
42. van Leer B., « Towards the ultimate conservative difference scheme: a second-order sequel to Godunov's method », J. Comp. Phys., vol. 32, p. 101-136, 1979.
43. Yee H., Upwind and symmetric shock-capturing schemes, Technical Memorandum no TM-89464, NASA, May, 1987.