• 수산해양기술연구
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• 제26권4호
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• pp.333-340
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• 1990

평판형과 만곡형전개판 주위에서의 유체특성을 파악하기 위하여 회유수조에서 수조기포법에 의한 하시화실험을 유속 0.05 및 0.1m/sec, 영각과 타임라인에 대해서 실시하였다. 그 결과를 요약하면 다음과 같다. 1. 만곡형전개판에서의 유선은 영각 20。까지는 균일한 분포를 이루다가 영각 25。에서 후면에 인접한 유선이 익현장의 1/2지점에서부터 작은 과가 발생되기 시작하고, 영각 30。에서는 익현자의 1.3지접에서 박리가 시작되며 인접한 유선은 전개판의 후면쪽으로 휘어들어가고, 그리고 영각 35。이상에서는 전연에서부터 박리가 시작되며 영각이 증가할수록 박리층이 증가하는 것으로 나타났다. 2. 평판형전개판에서는 영각 20。부터 전연에서 과와 박리가 발생하며, 박리층은 만곡형과 마찬가지로 영각에 비례하는 것으로 나타났다. 3. 후연에서 발생한 과의 크기가 전연의 것보다 약 2~3배 큰 것으로 나타났다. 4. 전개판의 후연에서 유선은 양 전개판 모두 전개판의 방향과 같은 방향으로 흐르다가 점차 유체흐름과 같은 방향이 되는 것으로 나타났다. 5. 전개판 전후면에서의 유속차는 영각 0。~30。에서 점차 증가하다가 영각 35。이상에서는 그 차가 비슷하게 나타났다. 6. 영각 20~30。에서 전후면의 유속차는 만곡형의 경우 후면의 유속이 전면보다 약 1.4~1.5배 빠르게 나타났으며, 평판형은 약 1.2배 빠르게 나타났다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 춘계 학술대회논문집
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• pp.79-82
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• 2007

The aerodynamic coefficients of Apollo capsule are calculated using a DSMC solver, SMILE, and the results agree very well with the data predicted by NASA. The aerodynamic characteristics of an orbital block which operates at high altitudes in the free molecule regime are also predicted. For the nominal flow conditions, the predicted aerodynamic force is very small since the dynamic pressure is extremely low. And the additional aerodynamic coefficients for the analysis of the attitude control are presented as the angle of attack and the side slip angle vary from $+45^{\circ}\;to\;-45^{\circ}$ of the nominal angle.

• 동력기계공학회지
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• 제20권1호
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• pp.69-74
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• 2016

The local heat transfer and pressure drops of developed turbulent flows in the convergent channels with square cross-sectional areas along the streamwise distance have been investigated experimentally. Four different parallel angled ribs (a = $30^{\circ}$, $45^{\circ}$, $60^{\circ}$, and $90^{\circ}$) are placed to the one sided wall only, respectively. The ribbed walls are manufactured with a fixed rib height (e)=10 mm and the ratio of rib spacing (p) to height (e) = 10. The measurement was run within the range of Reynolds numbers from 22,000 to 79,000. The result shows that the increases in the Nusselt numbers for the flow attack angles can be seen in the order of $30^{\circ}$, $45^{\circ}$, $60^{\circ}$ and $90^{\circ}$.

• 대한기계학회논문집B
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• 제25권5호
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• pp.713-721
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• 2001

Characteristics of the conical vortices on the roof corner of a rectangular prism have been investigated by using a PIV(Particle Image Velocimetry) technique. The Reynolds number based on the free stream velocity and the height of the model was 5.3$\times$10$^3$. The mean, instantaneous velocity vector fields, vorticity fields, and turbulent kinetic energy distribution were measured for two different angles of attack, 30$^{\circ}$and 45$^{\circ}$. The PIV measurements clearly observed not only the conical main vortex and the secondary vortex but also the tertiary vortex which is firstly reported in this paper. Asymmetric formation of the corner vortex for the case of 30$^{\circ}$angle of attack produces relatively the high magnitude of vorticity and turbulent kinetic energy around the bigger vortex which generates the peak suction pressure on the roof. Fairly symmetric features of the roof vortex are observed in the case of 45$^{\circ}$angle of attack, however, the dynamic characteristics are proved to be asymmetric due to the rectangular shape of the roof.

• 동력기계공학회지
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• 제19권5호
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• pp.32-37
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• 2015

The present study is to investigates the convective heat transfer characteristics and pressure drop inside the rib-roughened cooling passage of gas turbine blades. The divergent rectangular channel is fabricated with V-shaped ribs on one wall only and the inlet hydraulic diameter to outlet hydraulic diameter ratio($D_{ho}/D_{hi}$) of 1.49 is used. The current investigation has covered a Reynolds number (Re) range of 22,000~75,000, relative roughness height ($e/D_h$) of 0.1~0.2, and rib angle of attack (a) of $30^{\circ}$, $45^{\circ}$, and $60^{\circ}$ for a fixed relative pitch of 10. Results show that the Nusselt numbers are the greatest in the $60^{\circ}$-angled ribs; however, the total friction factors are the highest in the $30^{\circ}$-angled ribs.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2006년도 추계학술대회 논문집(제1권)
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• pp.45-49
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• 2006

물분사장치가 부착된 NACA-0021 익 주변의 흐름을 입자영상유속계를 이용하여 고찰하였다. $R_w=6.0261{\times}10^4$에서 영각(a)을 $0^{\circ}{\sim}35^{\circ}$로 변화시켜가며, 물분사 속도를 0[m/s], 9.2[m/s]의 2가지로 조절한 결과 익 후류영역에서는 박리 후 비정상적인(unsteady) 재순환 ${\cdot}$ 재부착 영역이 형성되었으며, 박리영역의 폭이 콴다 효과(Coanda effect)를 갖는 물분사로 인하여 최대 1/3만큼 감소하는 경향을 확인하였다. ?Nㄴ사가 없는 조건에서의 박리는 영각(a) $17^{\circ}{\sim}18^{\circ}$ 부근에서 시작되는 것이 관측되었으나, 물분사를 시켰을 경우 $20^{\circ}{\sim}21^{\circ}$에서 박리가 시작되는 것을 유동관측을 통해 알 수 있었다. 유동계측을 통해 익의 후연부(trailing edge)에서 생성되었던 와(vortex, eddy)가 물제트분사로 인해 소멸되는 것을 알 수 있었고, 영각이 작고 물분사 유속이 빠를수록 박리영역의 감소가 더욱 가속화됨을 알 수 있었다.

• 대한기계학회논문집B
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• 제26권9호
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• pp.1267-1275
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• 2002

An experimental study was performed to investigate adiabatic wall temperature and heat transfer coefficient around a module cooled by forced air flow. The flow angle of attack to the module were 0$^{\circ}$and 45$^{\circ}$. In the first method, inlet air flow(1~7m/s) and input power.(3, 5, 7W) were varied after a heated module was placed on an adiabatic floor(320$\times$550$\times$1㎣). An adiabatic wall temperature was determinated to use liquid crystal film. In the second method to determinate heat transfer coefficient, inlet air flow(1~7m/s) and the heat flux of rubber heater(0.031~0.062W/$m^2$) were varied after an adiabatic module was placed on rubber heater covering up an adiabatic floor. Additional information is visualized by an oil-film method of the surface flow on the floor and the module. Plots of $T_{ad}$ and $h_{ad}$ show marked effects of flow development from the module and dispersion of thermal wake near the module. Certain key features of the data set obtained by this investigation may serve as a benchmark for thermal-design codes based on CFD.

• 대한기계학회논문집B
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• 제23권5호
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• pp.678-686
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• 1999

The purpose of this work is to Investigate the pressure drop and the heat transfer characteristics in the channel of plate heat exchanger with crossed-discrete ribs. The flow is assumed to be three-dimensional, laminar and periodically fully developed. Computations have been carried out for angles of attack from $0^{\circ}$ to $90^{\circ}$ and ratios of rib height from 0.15 to 0.46 for various values of Reynolds and Prandtl numbers. The heat transfer was improved by inclined ribs generating helical vortices and secondary flows. The results show that the pressure drop has a maximum value at $70^{\circ}$ and the heat transfer has a maximum value at $45^{\circ}$. As the rib height increases, the pressure drop and the heat transfer increase quadratically, and the increasing rate of pressure drop is higher than that of the heat transfer. As Reynolds number increases, the pressure drop increases in proportion to the square of Reynolds number and the heat transfer increases linearly.

• 한국마린엔지니어링학회:학술대회논문집
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• 한국마린엔지니어링학회 2005년도 전기학술대회논문집
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• pp.1083-1090
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• 2005

Repeated ribs are used on heat exchange surfaces to promote turbulence and enhance convective heat transfer. Applications include fuel rods of gas-cooled nuclear reactors, inside cavities of turbine blades, and internal surfaces pipes used in heat exchangers. Despite the great number of literature papers, only few experimental data concern detailed distributions of friction factors and heat transfer coefficients in square channels varying the number of rough walls. This issue is tackled by investigating effects of different number of ribbed walls on heat transfer and friction characteristics in square channel. The rough wall have a 45$^{\circ}$ inclined square rib. Uniform heat flux is maintained on whole inner heat transfer channel area. The heat transfer coefficient and friction factor values increase with increasing the number of rough walls.

• 동력기계공학회지
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• 제9권1호
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• pp.30-35
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• 2005

Repeated ribs are used on heat exchanger surfaces to promote turbulence and to enhance convective heat transfer. Applications include fuel rods of gas-cooled nuclear reactors, inside cavities of turbine blades, and internal surfaces pipes used in heat exchangers. Despite the great number of literature papers, only few experimental data concerns detailed distributions of friction factors and heat transfer coefficients in square channels varying the number of rough walls. This issue was tackled by investigating effects of different number of ribbed walls on heat transfer and friction characteristics in square channel. The rough wall had a $45^{\circ}$ inclined square rib. Uniform heat flux was maintained on the whole inner heat transfer channel area. The heat transfer coefficient and friction factor values increased with increasing the number of rough walls.