• 대한기계학회논문집B
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• 제27권1호
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• pp.1-8
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• 2003

The heat transfer and flow measurements on a cylindrical pedestal mounted on a flat surface with a turbulent impinging jet were made. The experiments were made for the jet Reynolds number of Re = 23,000, the dimensionless nozzle-to-surface distance of L/d = 2~10, the dimensionless pedestal height of H/D = 0~1.5. Measurements of the surface temperature and the Nusselt number distributions on the plate surface were made using liquid crystal and shroud-transient technique. Flow measurements involve smoke flow visualization and the wall pressure coefficient. The results show that the wall pressure coefficient sharply decreases along the upper surface of the pedestal. However, the pressure increases when the fluid escapes from the pedestal and then collides on the plate surface. The secondary maxima in the Nusselt numbers occur in the region of 1.0 $\leq$ r/d $\leq$ 1.9. Their values for the case of H/D = 0.5 are maximum 80% higher than those for other cases. The formation of the secondary maxima may be attributed to the reattachment of flow on the plate surface which was separated at the edge of the pedestal.

• 대한기계학회논문집B
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• 제22권3호
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• pp.373-385
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• 1998

The local Nusselt numbers have been measured for a round turbulent jet impinging on the convex surface with and without rib. Liquid crystal/transient method was used to determine the Nusselt number distributions along the surface. The temperature on the surface was measured to within .+-.0.25 deg. C accuracy using liquid crystal and a digital color image processing system. The experiments were made for the jet Reynolds number (Re) 23,000, the dimensionless nozzle-to-surface distance (L/d) from 6 to 10, the dimensionless surface curvature (d/D) 0.056, and the various rib types (height(d$_{1}$) from 1 to 2 mm, pitch (p) from 6 to 32 mm). It was found that the average Nusselt numbers on the convex surface with rib are higher than those without rib, mainly due to an increase in the turbulent intensity caused by flow separation, recirculation and reattachment on the wall surface. In addition, we compared the results by the steady-state method using the gold-film Intrex with those by the transient method.

• 청정기술
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• 제16권3호
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• pp.213-219
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• 2010

볼텍스튜브는 고압의 가스를 이용하여 고온 가스와 저온 가스를 분리하거나 입자상 물질의 분리에 사용할 수 있는 장치이다. 이러한 볼텍스튜브의 에너지분리 특성과 물질분리 특성을 활용하여, 연소가스로부터 $CO_2$를 흡수하는 장치의 핵심부품으로 적용할 수 있다. 본 연구에서는 $CO_2$ 흡수용 볼텍스튜브의 기본설계 자료를 구축하기 위하여 에너지분리 성능실험을 수행하였다. 설계를 위한 기초 자료를 확보하기 위하여, 볼텍스 발생기의 오리피스 직경, 노즐면적비 및 튜브의 길이가 에너지분리 특성에 미치는 영향력을 실험을 통하여 분석하였다. 결과적으로 오리피스 직경이 볼텍스튜브의 성능에 지배적인 설계인자임을 확인하였으며, 노즐면적비와 튜브길이의 영향력은 미미하였다. 오리피스 직경이 작고(Dc=0.6D), 노즐면적비가 중간 이상(AR=0.14~0.16)이며, 튜브 길이가 긴 모델(L=16D)이 저온 출구 측과 고온 출구 측의 열전달에서 가장 우수한 성능을 나타내었다. 본 연구의 결과는 $CO_2$흡수용 $100Nm^3$/hr급 볼텍스튜브의 기본설계 자료로 활용될 예정이다. 볼텍스튜브를 적용한 $CO_2$흡수 공정을 적용하면 기존의 대형 흡수탑 대비 상당한 공간과 에너지의 절감 효과가 기대된다.

• 대한기계학회논문집B
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• 제23권6호
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• pp.734-743
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• 1999

The local Nusselt numbers have been measured for a round turbulent jet impinging on the concave surface with and without rib. Liquid crystal/transient method was used to determine the Nusselt number distributions along the surface. The temperature on the surface was measured using liquid crystal and a digital color image processing system. The experiments were made for the jet Reynolds number (Re) 23,000, the dimensionless nozzle-to-surface distance (L/d) from 4 to 10, the dimensionless surface curvature (d/D) 0.056, and the rib type (height ($d_1$) 0.2 cm, pitch (p) from 1.2 to 3.2 cm). It was founded that only when $L/d{\geq}6$, the average Nusselt numbers on the concave surface with rib are higher than those without rib, mainly due to an increase in the turbulent intensity caused by the effect of rib attached to the wall surface. It was realized that the rib attached to the concave surface may no longer enhance the heat transfer rate or even lowers it depending on the rib type and flow conditions. In addition, the results by the steady-state method using the gold-film Intrex were in good agreement with those by the transient shroud method.

• 대한기계학회논문집B
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• 제27권12호
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• pp.1673-1680
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• 2003

It is essential to operate chemical lasers with supersonic ejector system as the laser output power goes up. In this research, ejector design parameter study was carried out for optimal ejector design through understanding the ejector characteristics and design requirements for chemical lasers operating. Designed ejector was 3D annular type with 2$^{nd}$ -throat geometry and pressurized air was used for primary flow. Ejector design was carried out with two steps, quasi-1D gas dynamics was used for first design and commercial code was used to verify the first design. In this study, to get the effect of ejector geometry on its performance, three cases of primary nozzle area ratio and 2$^{nd}$ -throat cross sectional area and two cases of 2$^{nd}$ -throat L/D ratio experiments were carried out. Primary and secondary pressures were measured to get the mass flow rate ratio, minimum secondary pressure, ejector starting pressure and unstarting pressure at every case. In the result, better performance than design level was shown and optimal ejector design method for chemical lasers was obtained.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 추계학술대회논문집B
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• pp.278-284
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• 2000

The method of Impinging jet was applied lots of part in industrial field as a cooling of as gas turbine blade, a annealing of metal and plastic sheets, drying of textile, veneer paper, X-ray medical devices, laser weapons and electronic components. This study's main factor is reciprocating Jet impingement perpendicular to the heated Surface. We researched the effect of heat transfer and enhancement with pulsating air jet. The pulsating air jet has an improvement in pulsating Frequencies((f= 0.5, 1, 1.5, 3Hz) and nozzle-to-plate distances($l/d=\;2{\sim}4,\;6{\sim}8,\;4{\sim}6,\;8{\sim}10$).

• Carbon letters
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• 제2권2호
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• pp.99-104
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• 2001

Partial mesophase (PM) pitch precursor was prepared from fluidized catalytic cracking-decant oils (FCC-DO) by chemical reaction in the presence of $Br_2$. The PM pitch heated-treatment at $420^{\circ}C$ for 9 h exhibited the softening point of $297^{\circ}C$ with 23% yield, and 55% anisotropic content. The PM pitch precursor was melt-spun through circular nozzle by pressurized $N_2$, stabilized at $310^{\circ}C$, carbonized at $700^{\circ}C$, $1000^{\circ}C$, and $1200^{\circ}C$. The enough stabilization introduced 16.4% of the oxygen approximately. The stacking height ($L_{c002}$) and interlayer spacing ($d_{002}$) of the as-spun fibers were 4.58 nm and $3.45{\AA}$ and the value became minimum and maximum at $700^{\circ}C$ respectively in the carbonization procedure. The tensile strength increased with an increase in the heat treatment temperature exhibiting highest value of 750 MPa at $1200^{\circ}C$ carbonization.

• International Journal of Automotive Technology
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• 제7권2호
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• pp.139-143
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• 2006

As an automobile tends to be high grade, the needs for more luxurious interior and comfortable HVAC system are emerged. The defrosting ability is another major factor of the performances of HVAC system. The present work is to simulate the flow and the temperature field of cabin interior during the defrost mode. The three-dimensional incompressible Navier-Stokes equations and energy equation were solved on the multi blocked grid system by the iterative time marching method and AF scheme, respectively. The present computations were validated by the comparison of the temperature field of a driven cavity and velocity field of 1/5 model scale of an automobile. Generally good agreements were obtained. By the present computation, the complicated features of flow and temperature within the automotive cabin interior could be well understood.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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• pp.49-53
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• 2003

In this study, the geometric design parameters of ejector system were investigated. The critical parameters were primary nozzle area ratio, 2nd-throat cross sectional area and 2nd-throat L/D ratio. At every geometry cases, primary pressure and secondary pressure were measured simultaneously according to secondary mass flow rate. From the results, the ejector starting pressure, unstarting pressure and minimum secondary flow pressure were found and we got the effect of geometric parameters to ejector performance and the way to optimal design of ejector system for chemical lasers operating. Also the experiments of changing secondary flow temperature were carried out.

• 에너지공학
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• 제11권2호
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• pp.90-98
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• 2002

본 연구는 선회유동과 연소인자가 9.4L인 터보과급 디젤엔진의 성능과 배기가스특성에 미치는 영향을 실험적으로 고찰하였다. 일반적으로 디젤엔진의 연소과정에서 선회유동은 분사되고 있는 연료와 흡칩공기의 혼합을 촉진시켜 줌으로써 엔진성능을 향상시키는데 매우 중요한 인자가 된다. 특히 터보과급 디젤엔진에서는 실린더내의 고온.고압가스로 인하여 연비와 NO$_{x}$ 농도는 서로 상반관계를 가지므로 적절한 용량의 과급기선정으로 흡.배기시스템, 분사시스템 및 연소실의 설계 등을 고려할 필요가 있다. 본 연구의 결과로서, 정상유동실험을 통하여 선회비가 증가함으로써 평균유량계수가 감소하고, 반면에 걸프 펙터가 증가함을 알 수 있었다. 또한 엔진실험을 통하여 흡기포트의 선회비 2.43, 분사시기 BTDC 13$^{\circ}$ CA, 압축비 16, 리앤트란트 5$^{\circ}$형 연소실, 노즐분공경 $\Phi$0.28*6 및 과급기 GT40(압축기 A/R 0.58, 터빈 A/R 1.19)의 적용인자가 최적의 성능 및 배기가스를 만족시킬 수 있었다.