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유체-구조 연성해석을 이용한 능동/수동 유동제어방식이 결합된 고하중 축류 팬의 성능특성 연구

Investigation on Aerodynamic Performance of a Highly-Loaded Axial Fan with Active/Passive Flow Control Using FSI Analysis

  • 마상범 (인하대학교 대학원 기계공학과) ;
  • 김광용 (인하대학교 대학원 기계공학과) ;
  • 최재호 (한화테크윈 항공엔진개발센터) ;
  • 이원석 (한화테크윈 항공엔진개발센터)
  • Ma, Sang-Bum (Department of mechanical engineering, Graduate school, Inha University) ;
  • Kim, Kwang-Yong (Department of mechanical engineering, Graduate school, Inha University) ;
  • Choi, Jaeho (Aero Engine R&D Center, Hanwha Techwin) ;
  • Lee, Wonsuk (Aero Engine R&D Center, Hanwha Techwin)
  • 투고 : 2017.01.31
  • 심사 : 2017.02.28
  • 발행 : 2017.02.28

초록

An investigation on aerodynamic performance of a highly-loaded axial fan has been conducted to find the effects of tip injection and casing groove on aerodynamic performance in this study. Three-dimensional Reynolds-averaged Navier-Stokes equations with $k-{\varepsilon}$ turbulence model were used to analyze the fluid flow in the fan with Fluid-Structure Interaction (FSI) analysis. The hexahedral grid was used to construct computational domain, and the grid dependency test drew the optimal grid system. FSI analysis was also carried out to predict the deformation of rotor and stator blades, and the effect of deformation on the aerodynamic performance of axial fan was analyzed compared to the performance predicted without FSI analysis.

키워드

참고문헌

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