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PROPULSIVE PERFORMANCE AND VORTEX SHEDDING OF A FOIL IN FLAPPING MOTION 被引量:18

PROPULSIVE PERFORMANCE AND VORTEX SHEDDING OF A FOIL IN FLAPPING MOTION
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摘要 The propulsive performance and vortex shedding of oscillating foil, whichmimics biological locomotion, were numerically investigated. The objectives of this study were todeal with unsteady force, in particular thrust force, exerted on the foil in pitching and plungingmotions, and to explore the relation of the propulsive performance with vortex structures near thefoil and vortex shedding in the near wake. The two-dimensional incompressible Navier-Stokesequations in the vorticity and stream-function formulation were solved by fourth-order essentiallycompact finite difference schemes for the space derivatives and a fourth-order Runge-Kutta schemefor the time advancement. To reveal the mechanism of the propulsive performance, the unsteady forceand the shedding of the trailing- and leading-edge vortices of the foil were analyzed. The effectsof some typical factors, such as the frequency and amplitude of the oscillation, the phasedifference between the pitching and plunging motions, and the thickness ratio of the foil, on thevortex shedding and unsteady force were discussed. The propulsive performance and vortex shedding of oscillating foil, whichmimics biological locomotion, were numerically investigated. The objectives of this study were todeal with unsteady force, in particular thrust force, exerted on the foil in pitching and plungingmotions, and to explore the relation of the propulsive performance with vortex structures near thefoil and vortex shedding in the near wake. The two-dimensional incompressible Navier-Stokesequations in the vorticity and stream-function formulation were solved by fourth-order essentiallycompact finite difference schemes for the space derivatives and a fourth-order Runge-Kutta schemefor the time advancement. To reveal the mechanism of the propulsive performance, the unsteady forceand the shedding of the trailing- and leading-edge vortices of the foil were analyzed. The effectsof some typical factors, such as the frequency and amplitude of the oscillation, the phasedifference between the pitching and plunging motions, and the thickness ratio of the foil, on thevortex shedding and unsteady force were discussed.
出处 《Journal of Hydrodynamics》 SCIE EI CSCD 2003年第5期7-12,共6页 水动力学研究与进展B辑(英文版)
基金 ThisworkwassupportedbytheNationalNaturalScienceFoundationofChina (GrantNos:10125210,10 072063),theHundredTalentProgrammeoftheChineseAcademyofSciences,andtheInnovationProjectoftheChineseAcademyofSciences.(GrantNos:KJCX SWL04,KJCX2SW L2)
关键词 vortex dynamics vortex shedding thrust force unsteady flow flappingmotion vortex dynamics vortex shedding thrust force unsteady flow flappingmotion
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  • 1LU Xiyun and DALTON C. Calculation of the timing of vortex formation from an oscillating cylinder[J]. J Fluid Structures, 1996,10 : 527-541.
  • 2PHLIPS P J, EAST, R A and PRATT N H. An unsteady lifting line theory of flapping wings with application to the forward flight of birds[J]. J Fluid Mech ,1981,112: 97-125.
  • 3LIGHTHILL M J. Aquatic animal propulsion of high hydromechanical efficiency. [J]. J Fluid Mech ,1970,44: 265-301.
  • 4CHENG Jianyu, ZHUANG Lixian and TONG Binggang. Analysis of swimming 3-D waving plate[J]. J Fluid Mech, 1991, 232 : 341-355.
  • 5SMITH M J C, WILKIN, P J and WILLIAMS M H. The advances of an unsteady method in modeling the aerodynamic forces on rigid flapping wings[J]. J Exp Biol, 1996,199: 1073-1083.
  • 6TRIANTAFYLLOU M S , TRIANTAFYLLOU G S and GOPALKRISHNAN R. Wake mechanics forthrust generation in oscillation foils[J]. Phys Fluids,1991, 3: 12-26.
  • 7ANDERSON J M, STREITLIEN K, BARRETT D S and TRIANTAFYLLOU M S. Oscillating foils of high propulsive efficiency[J]. J Fluid Mech , 1998,360: 41-72.
  • 8ELLINGTON C P, BERG C Van Den, WILLMOTT A P and THOMAS A L R. Leading-edge vortices in insect flight[J]. Nature, 1996, 384: 626-630.
  • 9DICKINSON M H , LEHMANN F O and SANE S P. Wing rotation and the aerodynamic basis of insect flight[J]. Science,1999, 284: 1954-1960.
  • 10GUSTAFSON K E and LEBEN, R. Computation of dragonfly aerodynamics[J]. Comput Phys Commun ,1991, 65: 121-129.

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