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Hydrodynamic effects produced by oscillating foil in fluid

Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In the paper we presented the numerical results related to the unsteady effects produced by the oscillating foil in fluids. The paper was inspired by the studies over insects and birds fly. It was shown that by choosing of the frequency and amplitude of oscillations it can be generated the different kind of the vortex Karman street and this way control the drag, lift and thrust force exerted on the object. For numerical study vortex-in-cell method was used. We establish numerically relationship between Strouhal number amplitude of oscillations and vortices topology behind the oscillating foil by constructing the phase space diagram. The computational result are in consistent with the existent experimental data.
Słowa kluczowe
Rocznik
Strony
69--80
Opis fizyczny
Bibliogr. 18 poz., rys.,
Twórcy
autor
  • Wroclaw University of Technology, Department of Numerical Fluid Flow Modelling, Wybrzeże Wyspiańskiego 27, 50-370 Wroclaw
Bibliografia
  • [1] ANDERSON J., M., STREITLIEN K., BARRET D., S., TRIANTAFYLLOU M., S. Oscillating foils ofhigh propulsive efficiency J. Fluid. Mech, 360, 1998
  • [2] BECERRA SAGREDO Moment conserving Cardinal Splines Interpolation of Compact Supportfor Arbitrarily Spaced Data, Research Report No. -10 Zurich Switzerland, 2003
  • [3] COTTET G-H., KOUMOUTSAKOS P. Vortex Methods Theory and Practice, CambridgeUniversity Press, Cambridge, 2000
  • [4] GODOY-DIANA R., AIDER J-L.,WESFREID J., E. Transitions in the wake of a flapping foilPhysical Review E, 77, 2008
  • [5] GODOY-DIANA R., MARAIS C., AIDER J-L., WESFREID J., E. Model for the symmetry breaking of the reverse Benardvon Karman vortex street produced by flapping foil J. Fluid Mech., 622, 2009
  • [6] GUSTAFSON K., E., LEBEN R., FREYMUTH P. Visualization and computation of hovering mode, Vortex methods and vortex motion, 1991
  • [7] JONES K., D., DOHRING C., M., PLATZER M., F. Wake Structures Behind Plunging Airfoils: A Comparison of Numerical and Experimental Results, AIAA, 1996
  • [8] KOUMOUTSAKOS P., LEONARD A., PEPIN F. Boundary conditions for Viscous Vortex Methods, J. Comp. Phys., 113, 1994
  • [9] KUDELA H., MALECHA Z. M. Viscous flow modelling using the vortex particle method Task Quarterly, 13, 2009
  • [10] KUDELA H., KOZLOWSKI T. Vortex in cell method for exterior problems, J. Theor. Appl. Mech., 47, 2009
  • [11] PESKIN CH., S., MILLER L. A. When vortices stick: an aerodynamic transition in tiny insect flight, J. Exp. Biol., 207, 2004
  • [12] SHYY W., LIAN Y., TANG J., VIIERU D., LIU H. Aerodynamics of Low Reynolds Number Flyers Dover Publications, Dover Publications, Cambridge University Press, 2008
  • [13] THOMAS J., W. Numerical Partial Differential Equations: Finite Difference Methods, Springer, 1995
  • [14] WANG Z., J. The role of drag in insect hovering J. Exp. Biol., 207, 2004
  • [15] WANG Z., J., BIRCH J., M., DICKINSON M., H. Unsteady forces and flows in low reynolds number hovering flight: two-dimensional computations vs robotic wing experiments J. Exp. Biol., 207, 2000
  • [16] WEINAN E., JIAN-GUO LIU Vorticity Boundary conditions and Related Issues for Finite Difference schemes, J. Comp. Phys. 124, 66, 1996
  • [17] WU J. C. Theory for aerodynamics force and moment in viscous flows AIAA, 19, 1981
  • [18] WU J. Z., MA H.Y., ZHOU M.D. Vorticity and Vortex Dynamics, Springer, 2005
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BPW8-0019-0076
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