• Journal of Advanced Marine Engineering and Technology
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• 제26권4호
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• pp.485-492
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• 2002

The present study is aimed to reveal macroscopic aerodynamic characteristics of two-dimensional rectangular prisms with three aspect ratios(D/H=1, 2 and 3) and six angles of attack($0^{circ}, 10^{circ}, 13.5^{circ}, 20^{circ}, 30^{circ} and 45^{\circ}$). The Reynolds number is fixed as $1\times10^4$. The SOLA-based revised finite difference method for the conservation form on irregular grid was adopted as a new numerical method. Instantaneous flow patterns at $45^{\circ}$ in case of D/H=2 and D/H=3 show larger asymmetric wake development which is closely related to the sharp decrease of drag coefficients at higher angles of attack range. Vorticity propagation into enlarged wake region is conjectured to be responsible for this phenomenon. The Strouhal number is found to be sensitive to the angle of attack at higher aspect ratios(D/H=2 and 3).

• 설비공학논문집
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• 제14권6호
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• pp.477-484
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• 2002

A numerical investigation of the performance of the plate heat exchanger with rectangular winglet is conducted to examine the combined effect of vortex generator and louver fins. Velocity and temperature fields and spanwise averaged Nu and friction factor are presented. Enhancement of heat transfer and flow loss penalty is evident. A Parametric study of three factors (Re, angle of attack and louver angle) with levels of 5 (Re= 300, 500, 700, 900, 1100), 4($\alpha=15^{\circ}, 30^{\circ}, 45^{\circ}, 90^{\circ},$), and 4($\beta=0^{\circ}, 15^{\circ}, 30^{\circ}, 45^{\circ}$), respectively, indicates the performance defined by the ratio of heat transfer enhancement to flow loss penalty shows monotonic behavior for each parameter alone but the interactions between parameters is found to be considerable effect on the performance of heat exchanger and should be considered in design. The effect of stamping is also examined.

• International Journal of Aeronautical and Space Sciences
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• 제18권3호
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• pp.395-402
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• 2017

The local heat transfer and total pressure drops of developed turbulent flows in the ribbed rectangular convergent/divergent channels with ${\Lambda}/V-shaped$ ribs have been investigated experimentally. The channels have the exit hydraulic diameter ($D_{ho}$) to inlet hydraulic diameter ($D_{hi}$) ratios of 0.67 for convergence and 1.49 for divergence, respectively. The ${\Lambda}/V-shaped$ ribs with three different flow attack angles of $30^{\circ}$, $45^{\circ}$, and $60^{\circ}$ are manufactured with a fixed rib height (e) of 10 mm and the ratio of rib spacing (S) to height (e) of 10 on the walls. Thermal performances of the ribbed rectangular convergent/divergent channels are compared with the smooth straight tube under identical pumping power. The results show that the flow attack angle of $45^{\circ}$ with ${\Lambda}-shaped$ rib has the greatest thermal performance at all the Reynolds numbers studied in the convergent channel; whereas, the flow attack angle of $60^{\circ}$ with V-shaped rib has the greatest thermal performance over Reynolds number of 30,000 in the divergent channel.

• 한국터널지하공간학회 논문집
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• 제16권6호
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• pp.573-584
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• 2014

본 연구에서는 로드헤더 커팅헤드 설계의 기본 사항인 절삭조건에 따른 커터작용력의 변화를 살펴보는 기초 연구를 진행하기 위하여 연암 및 보통암을 대상으로 하는 슬림 코니컬커터를 사용하여 받음각과 커터관입깊이, 커터간격의 조건에 따른 선형절삭시험을 수행하였다. 각 시험조건에서 커터작용력인 연직력, 절삭력, 구동력을 측정하였고 그 측정결과의 평균값을 사용하여 분석을 실시하였다. S/d비와 비에너지의 관계, 관입깊이와 비에너지의 관계, S/d비와 커터작용력의 관계로부터 받음각이 $50^{\circ}$, 커터간격이 12 mm, 커터관입깊이가 9 mm인 조건이 모르타르시험체에 대한 최적의 절삭조건임을 확인할 수 있었다. 특히 받음각이 $50^{\circ}$인 경우가 $45^{\circ}$인 경우에 비해 장비사양 설계를 위해 더 효과적임을 알 수 있었다.

• Journal of Advanced Marine Engineering and Technology
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• 제26권4호
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• pp.439-449
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• 2002

Experimental investigations of the flow structure and heat transfer enhancement in a channel with a built-in circular cylinder and a wing-let type vortex generator are presented. Without any vortex generators, relatively low heat transfer takes place in the downstream of the circular cylinder where is a recirculation region with low velocity fluid is formed. However with a wing-let type longitudinal vortex generator in the wake region behind the cylinder, heat transfer in the region can be enhanced. In order to control the strength of longitudinal vortices, the angle of attack of the vortex generators is varied from $20^{circ} to 45^{\circ}$, but spacings between the vortex generations are fixed to be 5 mm. The 3-dimensional mean velocity field downstream of the vortex generator is measured by a five-hole pressure probe, and the hue-capturing method using thermochromatic liquid crystals has been used to provide the local distribution of the heat transfer coefficient. The vorticity field and streamwise velocity contour are obtained from the velocity field. Streamwise distributions of averaged Stanton number on the measurement planes show very similar trends for all the experimental cases($\beta=20^{circ}, 30^{circ} and 45^{\circ}$). Circulation strength and heat transfer coefficient have the maximum values when the angle of attack($\beta$) is $30^{\circ}$.

• Journal of Advanced Marine Engineering and Technology
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• 제39권6호
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• pp.609-613
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• 2015

축방향 거리에 따라 확대되는 정사각 채널에서 발달된 난류유동의 국부 난류 열전달과 압력강하를 실험적으로 조사하였다. 정사각 확대채널에 한 면에만 높이가 10 mm인 리브를 설치하였다. 리브의 충돌 각은 $30^{\circ}$, $45^{\circ}$, $60^{\circ}$ 그리고 $90^{\circ}$로 한 벽면에 만 설치하였다. 레이놀즈수가 22,000~79,000의 범위에서 실험을 수행하였다. 연구 결과 $45^{\circ}$의 리브 충돌각이 가장 우수한 열전달 성능을 보였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 춘계학술대회
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• pp.1453-1460
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• 2003

The present study investigates the effects of rib arrangements and aspect ratios of a rectangular duct simulating the cooling passage of a gas turbine blade. Two different V-shaped rib configurations are tested with the aspect ratios (W/H) of 3 to 6.82. One is the continuous V-shaped rib configuration with $60^{\circ}$ attack angle, and the other is the discrete V-shaped rib configuration with $45^{\circ}$ attack angle. The square ribs with the pitch to height ratio of 10.0 are installed on the test section in a parallel arrangement for both rib configurations. Reynolds numbers based on the hydraulic diameter are changed from 10,000 to 30,000. A naphthalene sublimation method is used to measure local heat/mass transfer coefficients. For the continuous V-shaped rib configuration, two pairs of counter-rotating vortices are generated in a duct, and high transfer region is formed at the center of the ribbed walls of the duct. However, for the discrete V-shaped rib configuration with $45^{\circ}$ attack angle, complex secondary flow patterns are generated in the duct due to its geometric feature, and more uniform heat/mass transfer distributions are obtained for all tested cases

• 한국수자원학회논문집
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• 제34권6호
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• pp.753-761
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• 2001

본 논문에서는 교각주위에서의 국부세굴 방지를 위한 사석 크기 및 접근각도 영향계수를 결정하기 위한 실험을 실시하였으며, 실험결과에 기초하여 사석크기 결정 공식과 접근각도 영향계수를 제안하였다. 접근각도 영향계수는 교각의 장폭비에 따라 다른 값을 보이며 교각에서의 접근각도가 증가됨에 따라 영향계수가 증가하는 경향을 보인다. 본 연구에서는 90%, 92.86%, 95%의 개도비와 1∼4의 장폭비를 가진 교각과 00, 150, 300, 450 및 600의 접근각도에 따른 실험을 실시하여 교각주위에서 국부 세굴 방지를 위한 사석크기를 결정하는 1개의 공식을 제안하였다. 본 논문에서 제안된 사석보호공의 크기 결정공식을 사용하여 사석을 크기를 산정한 결과와 기존의 6개의 사석 보호공 공식을 비교한 결과, 본 공식을 사용한 결과는 Richardson 공시을 이용하여 산정한 사석크기와 비슷한 결과를 나타내었다. 교각설치지점에 대한 흐름의 접근각도 영향계수가 고려된 본 논문에서 제안된 사석보호공 공식은 향후 국내 하천에서의 국부세굴 방지를 위한 사석보호공 설계에 폭넓게 사용될 수 있을 것으로 판단된다.

• Journal of Advanced Marine Engineering and Technology
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• 제25권5호
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• pp.1076-1085
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• 2001

Experimental investigations of the longitudinal vortices, which are produced by wing type vortex generators set up behind a circular cylinder in a rectangular channel, are presented. When the circular cylinder is set up in the rectangular channel, a horseshoe vortex is formed just upsteam of the circular cylinder. It generates a turbulent wake region behind the circular cylinder. Therefore, the region of the pressure loss behind the circular cylinder in increased and the size of the wake is small. These problems can be achieved by longitudinal vortices which are generated by wing-type vortex generator. In order to control the strength of longitudinal vortices, the angle of attack of the vortex generators is varied from 20 degree to 45, but the spacing between the vortex generators is fixed 6cm. The 3-dimensional mean velocity measurements are made using a five-hole probe. The vorticity field and streamwise velocity contour are obtained from the velocity field. The following results are obtained. Circulation strength is the maximum value when the angle of attack($\beta$) is $30^{\circ}$, and the vorticity field and streamwise velocity contour in case of $\beta$=$20^{\circ}$ show the trend similar to these in case of $\beta$=$30^{\circ}$, but do not in case of $\beta$=$45^{\circ}$.

• Journal of Advanced Marine Engineering and Technology
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• 제40권4호
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• pp.270-274
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• 2016

양 벽면이 수축되는 채널에서 ${\vee}/{\wedge}$형 리브의 각도가 열전달에 미치는 효과를 실험적으로 조사하였다. 한 벽면에만 설치된 ${\vee}/{\wedge}$형 리브의 충돌 각은 각각 $30^{\circ}$, $45^{\circ}$, $60^{\circ}$ 그리고 $90^{\circ}$이다. 리브의 높이(e)는 10 mm 그리고 리브 간격(p)과 높이(e)비는 10으로 제작하였다. 길이가 1,000 mm인 시험 부는 입구의 단면적은 $100mm{\times}100mm$, 출구는 $50mm{\times}100mm$으로 제작하였다. 레이놀즈수가 22,000에서 75,000까지의 범위에서 실험을 수행하였다. 연구결과 전체적으로 레이놀즈 수가 높을수록 누셀트 수가 컸고, ${\wedge}$형 $45^{\circ}$ 리브가 가장 누셀트 수가 컸다.