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직관과 연결된 나선관 입구영역의 층류 유동
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  • 직관과 연결된 나선관 입구영역의 층류 유동
저자명
김영인,박종호,Kim. Young-In,Park. Jong-Ho
간행물명
유체기계저널
권/호정보
2008년|11권 1호|pp.9-17 (9 pages)
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유체기계공업학회
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이 논문은 한국과학기술정보연구원과 논문 연계를 통해 무료로 제공되는 원문입니다.
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기타언어초록

A numerical study for three-dimensional laminar flow in the entrance region of helical tubes connected with straight ones is carried out to investigate the effects of Reynolds number, pitch and curvature ratio on the oscillation periods of the flow. The fully elliptic governing equations were solved by means of a finite volume method. The fully developed laminar flow boundary condition was applied at the straight tube inlet. This results cover a curvature ratio range of 1/10${sim}$1/320, a pitch range of 0.0${sim}$3.2, and a Reynolds number range of 62.5${sim}$2000. A comparison is made with previous experimental correlations and numerical data. The developments of velocity, local and average friction factors are discussed. The average friction factors are oscillatory in the entrance region of helical pipes. It has been found that the angle required for the flow to be similarly developed is most affected by the curvature ratio. The pitch and Reynolds number do not have any significant effect on the angle. The characteristic angle ${phi}_c(={phi}/sqrt{delta})$, or the characteristic length to diameter ratio $s_c(=lsqrt{delta} cos(atan{lambda})/d)$, can be useful to represent the development of flow in helical tubes. As the pitch increases and as the curvature ratio and Reynolds number decrease, the amplitude and the number of flow oscillations along the main streamwise direction decrease.