• 대한기계학회논문집B
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• 제28권9호
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• pp.1124-1132
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• 2004

The inverse problem of determining unknown inlet temperature in thermally developing, hydrodynamically developed two phase laminar flow in a parallel plate duct is considered. The inlet temperature profile is determined by measuring temperature in the flow field. No prior information is needed for the functional form of the inlet temperature profile. The inverse convection problem is solved by minimizing the objective function with regularization method. The conjugate gradient method as iterative method and the Tikhonov regularization method are employed. The effects of the functional form of inlet temperature, the number of measurement points and the measurement errors are investigated. The accuracy and efficiency of these two methods are compared and discussed.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2008년도 하계학술발표대회 논문집
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• pp.1172-1177
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• 2008

Diverging channel from gas burner exit to the inlet section of Heat Recovery Steam Generator (HRSG) has been re-designed for 1 MW steam supply and power generation system. Three different test geometries have been chosen for the numerical simulation. The existing design for 300 kW HRSG system (CASE B) has been improved by geometry and position changes of inlet guide vanes along with gas velocity entrance angle at the diverging channel inlet (CASE C). Both cases has been compared with the case where hot combustion gas is directly injected without any guide vanes (CASE A). Improved design shows overall uniform velocity and temperature distribution compared to existing design.

• 플랜트 저널
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• 제6권2호
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• pp.62-69
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• 2010

The stability of coal pulverizer in the 800 MW coal-fired plants is vital to maintain their performance. Thus, this study analyzed the uneven abrasion of the deflector and coal spillage due to the air velocity maldistribution in the vane wheel of a bowl-type pulverizer as it is a possible cause for problems of facility using pulverized coal. In addition, air flow in the underbowl of a bowl-type pulverizer was studied to check air velocity maldistribution in the vane wheel using numerical method. In an attempt to correct the maldistribution of air velocity, air flow of the modified duct vane was studied as enlarging the length of the duct vanes installed at the air inlet duct of the pulverizer and increasing the angle of inclination. It was found that modified duct vane make the velocity distribution at the vane wheel uniform. formed by the duct vanes installed at the air inlet duct of the pulverizer and swirling flow is the major factor in making the velocity distribution of vane wheel exit uniform. This can prevent the uneven abrasion of the deflector, which is one of the components inside the pulverizer and coal spillage.

• 동의생리병리학회지
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• 제16권3호
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• pp.464-471
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• 2002

Author applied several engineering methodologies to classical ultrasonic nebulizer to cope with it's demerits. After several trials and errors, we got the several meaningful results. To evaluate the modified ultrasonic nebulizer for inhalation toxicology of cadmium, author used light-scattering photometer. This paper is the one part of inhalation exposure systems for inhalation toxicology study of cadmium. According to the testing conditions, source temperature 50℃ and inlet-duct band temperature 150℃, aerosol generation results for sodium chloride and cadmium chloride were as followings: Coefficients of variation(CV) of sodium chloride and cadmium chloride for repeated trials were 3.38 and 4.77 for 10g, 2.47 and 5.02 for 5g, and 4.70 and 2.98 for 2.5g. All the CVs were within 10% of acceptance variability. Count Per Minute(CPM) changes of NaCl and CdCl₂ for 5 repeated trials were similar. CPM ratios of CdCl₂/NaCl were 1.13 for 10g, 0.76 for 5g, and 1.06 for 2.5g. Relative aerosol generation of cadmium chloride to sodium chloride was the highest in 10g. Efficiency increases of 24.50% for 5g NaCl, 14.91 % for 2.5g NaCl, and 16.48% for 2.5g CdCl₂ with respect to theoretical efficiency were observed but 0.04% efficiency decrease was observed in 5g CdC₂. According to the modifications of source temperature(20, 50, 70℃) and inlet-duct band temperature(20, 50, 100, 150, 200℃), aerosol generation results for NaCl and CdCl₂ were as followings: CPM trends for each quantity excepting 10g NaCl in inlet-duct band temperature 200℃ were similar, and the highest CPM was observed in source temperature 70℃ to each inlet-duct band temperature. The highest CPMs to 10, 5, and 2.5g NaCl were observed in source temperature 70℃ and inlet-duct band temperature 20℃. Aerosol generation of cadmium chloride was increased with the higher source temperature, excepting inlet-duct band temperature 200℃. The highest CPMs for 10, 5, and 2.5g CdCl₂ were observed in source temperature 70℃ and inlet-duct band temperature 20℃, and this trend was similar to NaCl aerosol generation The highest CPMs for 10, 5, and 2.5g CdCl₂ were observed in source temperature 70℃ and inlet-duct band temperature 20℃, and this result was similar to NaCl aerosol generation. Observed efficiencies of 5 and 2.5g NaCl were similar to ifs theoretical efficiency but -3.08% efficiency decrease of 5g CdCl₂, 17.47% efficiency increase of 2.5g CdCl₂ were observed. CPM ratio of CdCl₂/NaCl of 10g was different to 5 and 2.5g, and 2.5g ratio was higher than 5g ratio. In conclusion, to get maximum aerosol generation for NaCl and CdCl₂ will be the conditions that set the appropriate inlet-duct band temperature for each materials and increase the source temperature. Sodium chloride can be used to evaluate the performance and predict the concentration for cadmium aerosol in aerosol generator and inhalation exposure system.

• Journal of Advanced Marine Engineering and Technology
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• 제35권6호
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• pp.809-813
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• 2011

배열회수시스템 입구덕트의 3차원 난류유동을 수치시뮬레이션 하였다. 본 연구는 덕트의 루프각을 부분적으로 수정하여 유동의 형상효과를 해석하는 것이 목표이다. 비구조 격자를 가지고 나비에 스톡스 방정식을 유한체적법으로 풀어 유체동력학적인 현상을 규명하였다. 유적선, 속도벡터, 동압, 잔차 등으로 수렴 등을 조사하였다. 난류모형은 k-epsilon, k-omega, reynolds stress 및 RNG k-epsilon 이다. 선회 및 비선회 조건을 2개의 덕트에 적용하였고 계산결과를 활용하여 최적형상설계를 검토하였다.

• 오토저널
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• 제15권2호
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• pp.92-104
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• 1993

In the present study, the velocity profiles and entrance length of developing transitional pulsating flows are investigated both analytically and experimentally in the entrance region of a square duct. The systems of conservation equations for transitional pulsating flows in a square duct are solved analytically by linearizing the non-linear convective terms. Analytical solutions are obtained in the form of infinite series for velocity pofiles. The experimental study for the air flow in a square duct(40mm*40mm*4000mm) is carried out to measure velocity profiles and other parameters by using a hot-wire anemometer with a data acquisition and processing system. The distribution of velocity profiles( $u_{ps}$ / $u_{m,ta}$) in the decelerating period is higher than in the accelerating period. The distribution of the axial component of the axial component of velocity in the transitional flow is nearly uniform in the central region of the duct, and decrease rapidly near the wall. The entrance length correlation of the transitional pulsating flows in a square duct is obtained to be $L_{e}$/ $D_{h}$=0.83 $A_{1}$R $e_{ta}$ /(.omega. sup+1)$^{2}$TEX>

• 한국기계가공학회지
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• 제18권3호
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• pp.88-93
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• 2019

This study concerns the distributions of flow in an air conditioning duct used for a marine and oil drilling ship. From the results of carrying out flow analysis and structural analysis of a ventilation duct applied to a marine structure, the following conclusion could be gained. The pressure tended to increase as the flow velocity at the inlet increased and the pressure at the inlet increased. It was recognized that the pressure decreased due to the influence of a corrugated tube when it entered and exited from the duct. As a result of structural analysis, a higher train was generated at the corrugated tube compared with the duct. In addition, in the case of the internal pressure of 0.7MPa, which was the designed load, it was found that there was almost no influence as it was within 0.1mm.

• 한국추진공학회지
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• 제2권2호
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• pp.64-73
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• 1998

항공기용 엔진에는 압축기단들 사이에 스트럿을 포함하는 S자형 환형덕트가 존재하기도 한다. 이러한 엔진에서 S자형 덕트를 통과하는 유동은 볼록면과 오목면을 따라 가면서 가속과 감속이 이루어지고, 벽면에서의 경계층 성장으로 인해 유로폐쇄량이 증가한다. 이처럼 S자형 덕트의 영향으로 후방에 존재하는 압축기는 불균일한 축방향 속도분포에 따른 영향을 받게 된다. 따라서, 후방 압축기는 전방에 위치한 S자형 덕트의 영향을 충분히 고려하여 설계하여야 한다. S자형 덕트가 미치는 영향을 고려하여 설계된 원심압축기의 성능을 검증하고, S자형 덕트가 원심압축기 성능에 미치는 영향을 파악해보기 위해 압축기 입구에 S자형 환형덕트를 장착한 경우와 원통형 덕트를 장착한 경우에 대해 각각 성능시험을 수행하였다. 시험결과를 통해 입구에 S자형 덕트가 있는 경우에는 없는 경우보다 압축비 및 효율 등 압축기 성능이 저하되고, 쵸킹유량이 감소함을 알 수 있었다. 이러한 성능저하의 원인을 분석하기 위해 S자형 덕트를 포함하는 임펠러의 유동해석을 수행하였으며, 그 결과 성능저하의 원인은, S자형 덕트와 임펠러의 상호작용으로 설계시 예측했던 것보다 인듀서팁에서 상대마하수가 증가하였고, 영각이 감소하였기 때문임을 확인할 수 있었다.

• 한국분무공학회지
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• 제8권1호
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• pp.9-15
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• 2003

The liquid phase LPG injection (LPLI) system is considered as one of the next generation fuel supply systems for LPG, vehicles, since it can accomplish the higher power, higher efficiency, and lower emission characteristics than the existing mixer type fuel supply system. However, during the injection of liquid LPG fuel into the inlet duct of an engine, a large quantity of heat is extracted due to evaporation of fuel. A problem is that the moisture in the air freezes around the outlet of a nozzle, which is called icing Phenomenon. It may cause damage to the outlet nozzle of an injector. The frozen ice deposit detached from the nozzle also may cause a considerable damage to the inlet valve or valve seat. In this work, the experimental investigation of the icing phenomenon was carried out. The results showed that the icing phenomenon and process were mainly affected by humidity of inlet air instead of the air temperature in the inlet duct. Also, it was observed that the icing occurs first in the inlet of a nozzle, and grows considerably at the upper part of the nozzle inlet and the opposite side of the nozzle entrance. An LPG fuel, mainly consisting of butane, has lower latent heat of vaporization than that of propane, which is an advantage in controlling the icing phenomenon.

• 대한기계학회논문집 C: 기술과 교육
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• 제5권2호
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• pp.97-104
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• 2017

본 논문에서는 휠로더 냉각성능 평가를 위한 열유동해석의 효율성 향상과 비용 저감을 위해서 흡배기구 다공판형상을 Porous media 기법을 이용하여 단순화하고 해석 정도를 확인하였다. 여기서 Porous media에 적용된 다공판형상의 유동손실계수는 시험데이터를 바탕으로 정의하였다. 또한 다공판형상의 유동손실계수를 해석적으로 정의하기 위해 단위형상에 대한 압력손실을 계산하고 시험결과와 비교하였다. 마지막으로 휠로더 흡배기구를 단순화한 해석모델의 냉각해석 결과와 실차 방열시험 결과를 비교하였다. 이 연구를 통해 휠로더 흡배기구 단순화 해석기법의 적용 가능성을 확인하였으며 냉각성능 평가 및 개선 연구를 효과적으로 수행할 수 있는 기반을 마련하였다.