• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1997.04a
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• pp.63-72
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• 1997

본 논문은 분사제트 주위에 형성되는 와류를 조절하여 제트를 제어하기 위하여 유동가시화, 속도분포 및 난류성분을 측정하는 실험을 수행하였다. 와류를 조절하기 위한 방법으로 제트노즐 주위에 환형관을 설치하여 환형관으로부터 2차제트를 분사 또는 흡입함으로써 제트주위에 형성되는 전단류를 변화시켰다. 2차제트 분사시 주제트 주위에 형성되는 와류의 발달을 억제함으로써 제트 포텐셜코어의 길이가 아주 길어지는 제트유동을 얻을 수 있었다. 환형관으로부터 주제트주위의 유체를 흡입하는 경우 제트주위의 전단류가 흡입비 R=1.3∼l.65에서 대류불안정성에서 절대불안정성으로 바뀜으로써 형성된 와류가 하류에서 제트중심부까지 발전, 결합되는 것을 방지하여 더 긴포텐셜코어와 중심에서 낮은 난류강도를 얻었다. 위의 결과는 환형관 주위에 부착한 깃의 높이 변화에 따라서 변화하였는데, 이것은 깃이 환형관을 통한 흡입유동의 유로역할을 함으로써 제트밖으로부터 흡입되는 것을 방지할 수 있었다. 분사제트 벡터링을 위하여 제트노즐 주위의 환형관을 이등분하여 한쪽으로만 제트주위의 유동을 흡입함으로써 제트주위에 다른 전단류를 형성함과 동시에 Coanda효과를 이용하여 분사제트를 편향시켰다. 편향되는 정도 및 난류성분은 홉입속도 비에 따라서 크게 바뀌었다.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.10 no.2
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• pp.193-201
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• 1998

A heat exchanging system employing the impinging air jet is still widely used In the various fields due to its inherent merits that include the easiness in engineering applications and the high heat and/or mass transfer characteristics. The purpose of this study is to investigate the enhancement of heat transfer and flow characteristics by placing a turbulence promoters in front of heat exchanging surface. In this study, a series of circular rods are placed at the upstream of a flat plate heat exchanger that is located at potential core region(H/W=2) of a two-dimensional impinging air jet. Heat transfer enhancement is achieved by inserting turbulence promoter that results in the flow acceleration and disturbance of boundary layer. The average Nusselt number of the flat plate with the turbulence promoters is found to be around 1.42 times higher than that of the flat plate without the turbulence promoters. Based on the results of flow visualization with a smoke wire, it is confirmed that the heat transfer enhancement is caused by the flow separation and disturbance of boundary layer by inserting the turbulence promoter.

• Journal of the Korean Society of Propulsion Engineers
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• v.1 no.1
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• pp.33-45
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• 1997

Axisymmetric shear layers around a free jet is forced by co-flowing and counter-flowing secondary jets from/to an annular tube around the jet nozzle. The jet potential core extends far downstream with co-flowing secondary jets due to inhibited vortex developing and pairing. For counter-flowing cases, the axisymmetric shear layer around the jet transits from convective instability to absolute instability for velocity ratios R＝1.3～l.65 for the uniform velocity jets. Consequently, the jet potential core length increases and the turbulence level in the jet core is reduced significantly. The jets are controlled better with extension collars attached to the outer nozzle exit because the annular secondary flow is guided well by the extension collars. For the vectoring of jet, the annular tube around the jet is divided in two parts and the only one part is used for suction. The half suction makes the different shear layer around the jet and vectoring the jet by Coanda effect. The vectoring and turbulent components are varied significantly by the suction ratio. The experiments are carried out to investigate the characteristics of forced free jets using flow visualization, velocity and turbulence measurements.

• Journal of Advanced Marine Engineering and Technology
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• v.25 no.6
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• pp.1330-1335
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• 2001

A present study is the flow characteristics of impinging jet by PIV measurement and numerical analysis. The flow characteristics of impinging jet flow are affected greatly by nozz1e inlet velocity An circular sharp edged nozzle type($45^{\circ}$ ) was used to achieve uniform mean velocity at the nozz1e inlet, and its diameter is 10 mm(d). Therefore, the flow characteristics on the impinging jet can be changed largely by the control of main flow In this parent study, we investigate the effects of inlet velocity, its variable is nozzle inlet Reynolds numbers (Re=1500, 3000, 4500, 6000 and 7500)

• Proceedings of the Korean Society of Marine Engineers Conference
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• 2001.05a
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• pp.34-39
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• 2001

A present study is the flow characteristics of impinging jet by PIV measurement and numerical analysis. The flow characteristics of impinging jet flow are affected greatly by nozzle inlet velocity. An circular sharp edged nozzle type($45^{\circ}$) was used to achieve uniform mean velocity at the nozzle inlet, and its diameter is 10mm(d). Therefore, the flow characteristics on the impinging jet can be changed largely by the control of main flow. In this parent study, we investigate the effects of inlet velocity, its variable is nozzle inlet Reynolds numbers(Re=1500m 3000, 4500, 6000 and 7500)

• Solar Energy
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• v.15 no.1
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• pp.85-94
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• 1995

This research has been proceeded over the potential core region(H/B=2) of two-dimensional impinging air jet sytem, in which square rods(width of 6 mm) has been set up in front of heating surface in order to increase heat transfer. The objective of this research was to investigate the characteristics of heat transfer and air flow, in eases of the clearance from rods to heating surface(C=1, 2, 4, 6 mm) and the pitch between each rods(P=30, 40, 50 mm) changed. And this research compared the above with the experimentation without rods. As result, heat transfer performance was best under the condition of C=1mm, in case clearance changed, and there was no serious difference in the effect of heat transfer augmentation in the case of pitch of rods changed.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.24 no.3
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• pp.373-381
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• 2000

The flow and heat transfer characteristics on the impingement surface can be controlled by the change of vortex with the acoustic excitation, because the flow characteristics of an impinging jet are affected strongly by the vortices formed at the jet exit. To investigate the effects of acoustic excitation, we measured the velocity, turbulent intensity distributions for the free jet and local heat transfer coefficients on a impingement surface. As the acoustic excitation, subharmonic frequency of excited frequency plays an important role to the control of the jet flow. If the vortex pairings are promoted by the acoustic excitation, turbulence intensity of the jet flow is increased quickly. On the other hand if the vortex pairings are suppressed, the jet flow has low turbulence intensity at the center of the jet. Therefore, the low heat transfer rates are obtained on the impingement plate for a small nozzle-to-plate distance. However, it has high heat transfer rates at a large distance between the nozzle and plate due to the increasing of potential-core length.

• Proceedings of the Korea Water Resources Association Conference
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• 2007.05a
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• pp.229-235
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• 2007

관개나 수분수지 규명을 위한 기본적인 자료는 토양수분 함량이다. 그러나, 포장상태에서의 토양수분 함량은 직접 측정하는 것이 쉽지 않기 때문에 많은 경우 건조기를 이용한 중량수분 함량측정 방법을 이용하거나 토양수분 포텐셜 측정용인 텐시오미터를 이용한 토양수분의 에너지 특성을 관개에 활용하는 것이 현실이었다. 중량수분 함량은 시료를 채취해서 건조하기 때문에 시료채취 당시의 토양수분 함량을 아는 것이 어렵고, 토양수분 포텐셜은 에너지를 측정하는 것이기 때문에 이 역시 토양의 수분함량을 얻는 것이 불가능 하다. 따라서, 최근에 이런 측정상의 어려움을 극복하기 위해 여러 나라에서 포장에서의 토양수분 함량을 직접 측정하는 다양한 센서를 개발하고 있고 있다. 그 중 몇 가지는 현재 우리나라에 공급되고 있는데, 가격 등의 문제로 별로 알려져 있지는 않다. 센서는 현장에서 수분함량을 파악할 수 있는 장점이 있기 때문에 관개에 직접 적용이 가능하며 자동화시설이나 수분수지 모형 산정에도 활용할 수 있다. 본 시험은 우리나라에 소개되어 있는 몇 가지의 토양수분 측정용 센서를 현장에서 코어를 이용해 측정한 용적수분 함량과 비교하여 센서의 정확도나 이용 가능성을 검정하고자 하였다. 코어를 이용해 실측한 토양 용적수분 함량과 비교하고자 7종의 센서를 선택해 실험에 이용하였다. 가격이 비싼 것으로 알려진 TDR 형태의 센서가 2종이었으며, 나머지 5종은 FDR 형태의 센서였다. TDR 센서는 Soilmoisture사에서 제작한 MiniTrase와 Imko 사의 Trime이고, FDR은 Sentek사에서 개발한 EasyAG, EnviroSCAN과 Delta-T사에서 제작한 PR-1과 WET-2 및 Decagon사에서 제작한 $ECH_2O$ 센서였다. 실헙방법은 본량사양토인 포장에서 건조한 상태인 시험구와 물이 포화된 시험구를 만들어 놓고, 그곳에서 센서 종류별로, 측정 깊이별로 토양의 용적수분 함량을 측정하고, 센서로 측정한 위치 바로 옆에서 코어를 이용해 토양시료를 채취하고 이를 건조기에 건조해 용적수분 함량을 측정하였다. 비교결과 TDR인 MiniTrase가 결정계수$(r^2)$가 0.964이고 표준오차(SE)가 0.01로 좋은 결과를 보여줬고 WET-2가 $r^2$와 SE가 0.932와 0.013이였으며 EasyAG는 0.877과 0.0211, EnviroSCAN은 0.803과 0.0259의 값을 보였다. 일반적으로 토양수분 함량 측정오차가 1% 미만인 센서가 정확한 수분함량 해석을 유도할 것이지만 위의 센서 중 MiniTrase를 비롯한 4개의 센서 정도가 토양의 수분 함량을 측정하는데 유용할 것이라는 결론을 얻었다.

• Proceedings of the KSME Conference
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• 2003.04a
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• pp.2031-2036
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• 2003

High-pressurized jet is widely using in industrial works. however, few papers studied on the performances or characteristics on that kind of nozzles. And in this study, some flow characteristics with the variation of nozzle aspect ratios such as mean velocity distributions, momentum variations along the center line have been experimentally investigated. As the results, some semi-empirical correlations of profiles of pressure and mean velocity distributions, momentum conservations with the nozzle aspect ratios are formulated. It is expected that these empirical formula can be applied for the random estimations of nozzle performances.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.28 no.2
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• pp.135-145
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• 2004

An experimental study is conducted to investigate the flow and heat transfer characteristics of a multi-tube inserted impinging jet. Four different multi-tube devices are tested for various nozzle-to-plate distance. Flow visualization by smoke-wire method and velocity measurements using a hot-wire anemometer are applied to analyze the flow characteristics of the multi-tube insert impinging jet. The local heat transfer coefficients of the multi-tube inserted impinging jet on the impingement surface are measured and the results are compared to those of the conventional jet. In multi-tube inserted system the multi-tube length plays an important role in the flow and heat transfer characteristics of the jet flow. With multi-tube insert of I3d4 and I6d4 which has relatively longer tube length than the multi-tube-exit of I3d1 and I6d1, the flow maintains its increased velocity far downstream due to interaction between adjacent flows. For the small H/D of 4, the local heat transfer coefficients of multi-tube inserted impinging jet are much higher than those of the conventional jet because the flow has higher velocity and turbulent intensity by the use of the multi-tube device. At large gap distance of H/D=12, also higher heat transfer rates are obtained by installing multi-tube insert except multi-tube insert of I3d1.