Asymmetric sinusoidal motion effect on aerodynamics of a plunging airfoil

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Abstract

The effect of asymmetric sinusoidal motion on plunging airfoil aerodynamics was studied by numerical simulations for 2-D flow around a NACA0012 airfoil at Re=1.35×105. Various unsteady parameters (nondimensional plunging amplitude, h, reduced frequency, k) were applied to investigate the effect of asymmetry parameter S on the instantaneous force coefficient and flow pattern. It is found that more thrust can be generated by asymmetric sinusoidal plunging motion compared with pure sinusoidal case, and the thrust force generated increases with asymmetry. Moreover, a significant difference in the wake pattern at different values of S is observed. The trailing wake is displaced downward relative to the free stream for S less than 0.5, and displaced upward for S larger than 0.5.

Original languageEnglish
Title of host publicationAdvances in Manufacturing Science and Engineering
Pages1410-1413
Number of pages4
DOIs
StatePublished - 2013
Event4th International Conference on Manufacturing Science and Engineering, ICMSE 2013 - Dalian, China
Duration: 30 Mar 201331 Mar 2013

Publication series

NameAdvanced Materials Research
Volume712-715
ISSN (Print)1022-6680

Conference

Conference4th International Conference on Manufacturing Science and Engineering, ICMSE 2013
Country/TerritoryChina
CityDalian
Period30/03/1331/03/13

Keywords

  • Asymmetric sinusoidal motion
  • Navier-stokes simulations
  • Plunging airfoil
  • Propulsion
  • Unsteady aerodynamics

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