• DocumentCode
    2042391
  • Title

    Numerical and experimental investigation of the hydrodynamics of flapping foil added in-line motion

  • Author

    Fujuan Liu ; Weishan Chen ; Kai Zhou

  • Author_Institution
    Dept. of Mech. & Electron. Eng., Harbin Inst. of Technol., Harbin, China
  • fYear
    2015
  • fDate
    2-5 Aug. 2015
  • Firstpage
    976
  • Lastpage
    981
  • Abstract
    The flapping foil based on bionics is a sort of simplified model which imitates the motion of the wings or fins of animals. Based on the backgrounds of underwater vehicle with high capabilities of propulsion, the hydrodynamics of flapping foil added in-line motion is numerical and experimental investigated in this paper. We simulate this 3 DOF motion in the method of computational fluid dynamics. The synthetic effect of the heave amplitude, Strouhal number, attack angle, and the stroke angle on the propulsive efficiency are investigated by the response surface methodology (RSM). We obtain a prediction model of the propulsive efficiency depended on the four parameters and design a 3 DOF experimental setup with the aim of investigating the propulsion mechanism of the flapping hydrofoils and analysis the hydrodynamic forces generated on the hydrofoils.
  • Keywords
    hydrodynamics; propulsion; response surface methodology; 3 DOF motion; RSM; Strouhal number; animals; attack angle; bionics; computational fluid dynamics; fins; flapping foil added in-line motion; flapping hydrofoils; heave amplitude; hydrodynamic forces; hydrodynamics; propulsion mechanism; propulsive efficiency; response surface methodology; stroke angle; underwater vehicle; wings; Encoding; Force; Hydrodynamics; Mathematical model; Predictive models; Propulsion; Response surface methodology; Propulsion; experimental setup; flapping foil; response surface methodology;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronics and Automation (ICMA), 2015 IEEE International Conference on
  • Conference_Location
    Beijing
  • Print_ISBN
    978-1-4799-7097-1
  • Type

    conf

  • DOI
    10.1109/ICMA.2015.7237618
  • Filename
    7237618