Journal of the Korean Society for Aeronautical & Space Sciences (한국항공우주학회지)

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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A Study on Hear Transfer around a Sharp Fin in Supersonic Flow

초음속 유동내 돌출된 핀 근방의 열전달 연구

  • 송지운 (연세대학교 기계공학부 대학원) ;
  • 유만선 (연세대학교 산업기술연구소) ;
  • 조형희 (연세대학교 기계공학부)
  • Published : 2007.10.31
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Abstract

Heat transfer characteristic near a sharp fin was studied in a supersonic flow. Mach number and the Reynolds number were 3 and $5{\times}10^7$ respectively. Infra-red thermography was used to obtain the variation of surface heat transfer coefficient distribution. The angles of attack were ranged from $12.5^{\circ}$ to $20^{\circ}$ and the numerical analysis and the oil flow method were conducted to understand flow fields near a sharp fin.

초음속 유동장 내에 돌출된 핀에 의해 발생하는 바닥면의 열전달 특성 변화 연구를 수행하였다. 마하수가 3이고, 레이놀즈수가 $5{\times}10^7$인 초음속 유동내에 받음각이 $12.5^{\circ}$부터 $20^{\circ}$인 기울어지지 않은 형태의 선단이 날카로운 핀(sharp fin)을 돌출시켜 충격파를 발생시켰다. 이로 인해 생기는 바닥면의 열전달 계수의 변화를 적외선 카메라를 이용한 온도 분포의 측정을 이용하여 계산하였다. 또한 바닥면 유동의 흐름을 파악하기 위해 수치해석과 유막법이 수행되었다.

Keywords

References

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