• Transactions of the Korean Society of Mechanical Engineers B
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• v.38 no.11
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• pp.881-887
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• 2014

This paper presents numerical study on flow and heat transfer characteristics in micro-gap plate heat exchanger. In particular, we investigate the effect of flow inertia on the flow distribution from single main channel to multiple parallel micro-gaps. The flow regime of the main channel is varied from laminar regime (Reynolds number of 100) to turbulent regime (Reynolds number of 10000) by changing the flow rate, and non-uniformity of the flow distribution and temperature field is evaluated quantitatively based on the standard deviation. The flow distribution is found to be significantly affected by not only the header design but also the flow rate of the main channel. It is also observed that the non-uniformity of the temperature field has its maximum at the intermediate flow regime.

• 유체기계공업학회:학술대회논문집
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• 2004.12a
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• pp.65-69
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• 2004

In the present work, characteristics of an axial flow fan haying distorted inlet flow produced by hub cap are investigated. The distorted inlet flow is generated by the shape of hub cap installed in front of the axial flow fan. Two different cases of hub cap geometry are analyzed to verify the influence of flow distortion. The flow fields are analyzed numerically by solving steady form of three-dimensional Reynolds-averaged Wavier-Stokes equation and standard k-$\epsilon$ model is used for a turbulence closure. The results obtained from the numerical simulation are compared to those from experimental measurements. It is found that the overall performance of the axial flow fan is increased by reducing the flow distortion at the hub. Detailed characteristics of the flow fields of two different geometric conditions are also discussed.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.13 no.11
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• pp.1114-1124
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• 2001

The application of carbon dioxide as an attractive natural working fluid in air cooling and heating system is increasingly important in view of the CFC substitution problem. The thermal performance of compact evaporator was analyzed using section-by-section method. The effects of the two-dimensional nonuniformity of air flow through the evaporator is presented. The detrimental effect of the aid flaw nonuniformity on the thermal performance of the evaporator is found to be significant for many typical applications. It is shown that total heat transfer rate of evaporator using $CO_2$ is higher than that using R134a at the simulation conditions.

• 유체기계공업학회:학술대회논문집
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• 2003.12a
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• pp.476-481
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• 2003

In this paper, the effect of circumferential inlet distortion on performance and stall has been experimentally investigated in a high-speed centrifugal compressor, comparing distorted cases with undistorted one. The performance of compressor was slightly deteriorated by defect of inlet static pressure which is caused by the circumferential inlet distortion. As stall was fully developed the inlet distortion did not affect the number of stall cell and the propagation velocity. It also did not affect stall inception at 40,000 and 50,000 rpm. However stall occurred at the lower flow rate for distorted flow at 60,000 rpm. For 50,000 rpm a unexpected phenomenon occurred : stall occurred first and then it disappeared.

• 한국항공운항학회:학술대회논문집
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• 2004.11a
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• pp.202-210
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• 2004

• Journal of the Korean Society of Propulsion Engineers
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• v.24 no.2
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• pp.28-34
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• 2020

In order to relieve the burden of the rear ablative material, the combustion test of the solid rocket motor with the forward deployed multi-pin grain design was successfully performed twice. However, after disassembling the solid rocket motor, a non-uniform ablation pattern was found in the rear ablative material. Periodic repetition of local and regional ablation was measured precisely. Two-dimensional flow and eddy flow, created by the uneven main-pin flow hitting the rear ablative material, were identified as the cause of non-uniform ablation. In addition. when the rear pins were removed, the possibility of securing the soundness of the rear ablative material was confirmed as the average flow velocity and the standard deviation were lowered.

• Journal of the KSME
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• v.32 no.3
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• pp.247-254
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• 1992

이 글에서는 고충아파트에서 층간 열공급의 불균일성이 발생하는 원인을 설명하였고 이 불균일 성을 해소시키는 새로운 열공급 설비 기술을 설명하였으며 그 내용들에 대한 결론은 다음과 같다. (1) 온수 난방 고층아파트의 층간 열공급의 불균일성은 온수공급관과 회수관의 정수압력의 차 이에 의한 유동저항에 의해서 발생한다. (2) 다구역배관망 시스템은 온수공급관과 회수관의 정수압력의 차이에 의해 발생하는 열공급 불균일성의 해소에 거의 기여하지 못한다. (3) 연속난방방식에서 서모스타트의 설치는 각세대의 열공급을 균일하게 할 수 있고 에너지 절 약면에서 가장 유리한 방식이나 고장의 위험성이 가장 크며, 운전의 미숙에 의한 열공급 제어의 불균일성을 초래하기 쉬우며 외기온도가 매우 낮으면 층간 열공급제어가 되지 않을 수 있어서 자동유량조절밸브를 병용하거나 온수공급압력을 충분히 크게 할 필요가 있다. (4) 자동유량조절밸브에 부착하면 단구역 배관망 시스템에서도 층간의 유량공급의 불균일성을 없앨 수 있으나 순환 펌프유량이 부족하면 밸브의 자동유량조절 기능이 상실된다. (5) 수동유량조절밸브는 TAB에 의해서 충간의 유량을 균일하게 조절할 수 있으나 펌프 성능변화 관부식 등이 발생하면 TAB를 다시 할 필요가 발생할 수 있다. 그러나 밸브의 고장이 적고 유 동저항을 적게 발생시키며 한 개의 밸브로 조절할 수 있는 유량의 범위가 큰 점에서는 가장 유 리하다.

• Journal of Energy Engineering
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• v.17 no.3
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• pp.161-166
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• 2008

The purpose of this study is to apprehend the behavior of exhaust gas flow from gas turbine during part load operation in Heat Recovery Steam Generator. As a first step of this work, internal flow characteristics according to HRSG types were examined by CFD analysis. Next step, tube temperature according to gas turbine 53% and 100% load conditions were calculated by results of CFD and those were compared with temperature data gathered from real plant. Finally, thermal performance due to part load operation was calculated to estimate the influence of heat transfer in superheater. In addition, new type of device is suggested to eliminate the uneven temperature distribution of tubes during part load operation.

• Proceedings of the Korean Vacuum Society Conference
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• 1993.02a
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• pp.38-40
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• 1993

급속 열처리 시스템내에서의 비정상상태 온도분포, 가스유동형태, 웨이퍼내 열응력등을 여러 가지 작동조건하에서 2차원 유한 차분법으로 계산하였다. 계산결과는 실험에서 얻은 에피성장률 데이터와 비교 검증하였다. RTpp내 가스 유동이나 온도분포는 압력 및 주위 구성요소에 크게 의존하는 반면, 웨이퍼의 온도분포는 wafer edge loss가 큰 고온에서 온도 불균일도가 가장 크다. 저온에서는 대류에 의한 열 손실이 웨이퍼내의 온도 불균일도에 큰 영향을 미치고 있다. 웨이퍼상의 열응력을 가장 크게 받는 시점은 transient condition에서 나타났다.

• Journal of the KSME
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• v.56 no.9
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• pp.54-57
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• 2016

로켓연소기는 수백 개의 분사기로 구성된 연소실에서 연소반응이 발생하게 된다. 이때 구조적인 특성으로 난류유동, 밀도, 온도 등의 변화가 매우 불균일한 3차원적인 분포를 가지게 된다. 이러한 불균일한 분포에 의해 발생되는 압력의 시간변화가 연소기의 고유진동수와 일치될 경우 공진이 발생하게 되어 폭발이 발생하게 된다. 이러한 현상을 연소불안정이라 하고 이글에서는 관련된 연구의 동향을 소개하고자 한다.