본 연구에서는 간척지 풍 환경 특성에 따른 온실의 환 기효율 분석 연구에 대한 기초연구로서 단동 양지붕형온실을 대상으로 간척지 풍 환경을 적용한 풍동실험 및 PIV 실험을 수행하여 풍속, 환기방식에 다른 온실 내부 공기유동 분석을 수행하였다. 실질적인 간척지 풍환경 적용을 위하여 ESDU 프로그램을 활용하여 풍속 및 난류 프로파일을 설계하여 풍동실험에 적용하였으며 구현 결과 ESDU 대비 5%의 오차 및 상관계수 0.96이 도출 되었으며 적절한 오차범위라 판단하여 이를 기준으로 실험을 진행하였다. 벡터장, 컨투어장을 통한 분석 결과, 풍상측에서 유입 되는 공기가 온실 하부로 주기류층을 형성하고 온실 상부로는 주풍방향과 반대방향으로 다소 약한 기류를 형성 하는 것으로 측정되었다. 이는 환기 시, 온실 하부영역 이 가장 환기가 원활한 위치이며 후류가 형성되는 상부 영역은 저속의 순환구역으로 온실 내부에 있어 환기에 가장 취약한 위치임을 알 수 있었다. 또한 외부풍속 대비 온실 유입구 유속의 경우 상이하게 나타난 바, 이는 차후 환기량이나 환기효율의 산정에 있어 보다 실질적인 수치가 될 것으로 사료된다. 온실 내부 중앙부 기준 수직 높이에 대한 높이별 유속 수치 도출 및 분석결과, 풍속의 증가율에 비례하여 내부 유속 분포 수치 또한 비례해서 증가하는 것을 알 수 있었다. 환기방식에 따른 내부 유속 저감 비율은 측창 환기, 측창-천창 환기의 경우 각각 약 40%, 30%로 나타났으며 측창-천창 환기조건에서는 천창을 추가적으로 개방 함으로써 공기의 유입되는 면적이 증감함에 따라 온실을 기준으로 발생되는 부압이 감소하여 오히려 측창 환기조 건보다 더 큰 유속 수치가 도출된 것으로 사료된다. 이는 차후 질량교체 환기량, 추적가스 감쇠법 등의 방법을 통한 환기량 산정에 있어 환기방식에 따른 환기량의 변화양상에 대한 분석을 추가적으로 수행할 필요성을 지니는 자료로 판단된다. 본 연구를 통하여 도출된 결과를 바탕으로 전산유체 역학(Computational Fluid Dynamics, CFD) 시뮬레이션에 접목하여 앞서 도출된 정량적인 높이별 유속 수치 및 정성적 유동분포를 기준으로 검증 및 정확도 향상을 통한 환기분석 모델을 설계하고자 하였다. 온실 내부의 공기유동에 따른 보다 실질적인 환기 척도를 도출하여 다양한 온실형태별, 환경조건별, 환기방식별 환기경향 분석 및 예측이 가능할 것으로 전망되며 시뮬레이션을 활용한 온실 체적 전체 및 구역별 환기량을 예측하여 환기 취약 구역을 파악, 보완할 수 있을 것으로 기대된다.

In this paper, we have studied about the Energy Storage System (ESS) for renewable energy such as wind and solar energy by using Battery Energy Storage System (BESS). The BESS, by using Li-Ion battery, takes the advantage of high energy density. The ESS is composed of a large number of the battery. It is necessary to stabilize the temperature of the battery in order to improve the performance of the ESS. To improve the performance of ESS, Using as a program to analysis the container internal flow and heat distribution. The use of the battery to the stable and suggest in the initial battery array design of the heat concentration phenomenon in the battery array

This study is done as a comparison analysis on existing studies on analysis and interpretations of solenoids. When there is no power in a solenoid valve, a flow passage is formed from a pressurized ports, Pc, to Ps, which are connected to a crankcase of a pressurizer. An inlet to Pc port is varied in three different sizes: 3.8 ㎜(Type-1), 4.0 ㎜(Type-2) and 4.2 ㎜(Type-3). It is determined that there will be changes in coolant flow into the solenoid valve and the flow properties from Pc port to Ps port are compared and analyzed. As the results, the flow demonstrates the maximum speed of 500 ㎧, 46 ㎧ and 433 ㎧ with 0.2 ㎫ for the inflow pressure and the maximum speed of 1400 ㎧, 129 ㎧ and 1200 ㎧ with 1.5 ㎫ for the inflow pressure.

In this paper, we analyzed the characteristics of the mass flow rate and velocity of the refrigerant in response to a change in the number of holes and the diameter size(Type-1～4) of the valve guide refrigerant to flow from Pc to Ps when the pressure is constant. Type-1 is 40% higher mass flow flowing in the direction of Ps as compared with the Pc mass flow rate. Type-2 is 64% higher mass flow flowing in the direction of Ps as compared with the Pc mass flow rate. Type-3 is 50% higher mass flow flowing in the direction of Ps as compared with the Pc mass flow rate. Type-4 is 47% higher mass flow flowing in the direction of Ps as compared with the Pc mass flow rate.

This paper carried out a comparative analysis with papers on the analysis and analytic research of conventional solenoid. In case the current of solenoid valve is cut off, a flow path is formed from pressure port (Pc) connected with the crankcase of compressor to Ps port. At this time, the size of Pc port hole was so adjusted (Type-2) that it was smaller than 4.0mm(Type-1) of original hole by 0.2mm. After that, it was thought that an effect would be produced on the flow change of refrigerant which came into the solenoid vale, therefore the flow characteristics in moving from Pc port to Ps port was predicted and comparatively analyzed. According to the results of flow analysis, a velocity of approximately 46m/s and 129m/s was shown at the maximum in case of 0.2 and 1.5 MPa in Type-1, and the maximum velocity of approximately 500m/s and 1400m/s was shown in case of Type-2.

In this study, numerical simulation has been conducted to investigate flow characteristics in air supply room for container vessels by a 3-dimension numerical simulation. A commercial CFD program, FLUENT, is used on the analysis. It is shown that the air supply efficiency in this room can be improved by changing position of axial fan, even though other conditions still remain unchanged.

Numerical analysis of the electric vehicle battery was performed for the optimization of the thermal management under various operating conditions. For the analysis of internal flow and temperature distributions under the different operating conditions of battery, the battery system which was packed 18 battery cell with -25℃∼ 65℃ operating temperature range was considered, and the air flow rate, velocity, and ambient temperature conditions were varied and compared. It was revealed that the cooling system for battery was necessary to maintain its performance for hot ambient conditions. Especially, in this condition, at least 90m3/h of air flow rate are required to maintain the module temperature under 40℃. However, heating system of battery for cold ambient conditions doesn't need.

In this paper, the current of ECV block is connected to compressor crankcase on which the Pc port of Ps port Euro is formed(Type-1). Pc Port Internal Bellows are supposed to be affected by changes at the flow of refrigerant to the solenoid valve inside inhalation. There is Ps port at the direction of flow characteristic in predicting and analyzing. At suction pressures of 0.2MPa and 1.5MPa, maximum flow rates become 46m/s and 129m/s respectively. The refrigerant is discharged by compressor rotation around the axis of rotation from the inflow of port(Pd)(Type-2). By predicting and analyzing inlet flow, suction pressures become 2.7MPa and 3.6 MPa when maximum flow rates of 177.5m/s and 205m/s are affected on Pc ports of Euros with pressures of 1.2KPa and 3.8KPa respectively. This study result can be applied as the basic data for design of ECV.

이 연구에서는 정사각 단면을 갖는 덕트 내부에 원심력의 영향을 받는 유동의 천이특성을 실험 및 수치적으로 규명하였다. 실험적 연구로서 레이저도플러 속도계를 이용하여 축방향속도를 측정하였고, 상용소프트웨어인 플루언트를 이용한 전산유체 시뮬레이션으로 천이특성을 고찰하였다. 유동의 발달은 딘수와 굽힘각에 의존한다는 사실을 알 수 있었으며 덕트의 중앙에서의 속도분포는 원심력 때문에 내외벽보다 낮은 값을 나타내었다.

본 연구는 콘덴싱 보일러 내부에 들어가는 원심 터보형 송풍기의 성능 향상 및 그 유동특성을 파악하고자 하였다. 보일러는 연소를 위해 반드시 필요한 가스와 공기의 양이 조절되어야하며, 이를 위해 송풍기는 보일러 내부의 한정된 영역을 차지한다. 한정된 영역에서 최적의 효율을 얻기 위해서는 케이싱 및 임펠러의 형상을 변경하는 것이 일반적으로 사용되며, 형상변화에 따른 입/출구압력, 유량, 임펠러의 토크 등의 성능특성을 파악하였다. MRF(Multiple Rotating Frame)기법 및 k-ù SST 난류 모델을 적용하여 회전 임펠러에 대한 수치해석을 수행하였으며, 형상의 변경에 따라 송풍기의 성능특성 및 최적화된 설계형상을 제안하였고, 압력측정실험을 통해 그 결과를 검증하였다.

In this study, a experimental work to investigate the influence of a turbulent wake flow on the velocity distribution of a diffuser with PIV method. The turbulent wake is generated by a rectangular prism, which is installed at the inlet of a diffuser. The results show that the velocity recovery of the subsonic diffuser is dependent on the height and location of rectangular prism. It is found that a certain height of the rectangular prism to generate the turbulent wake give a better velocity recovery, compared with no rectangular prism.

With continuous industrial development, the types, and amount of particulate matter (PM) have been increasing. Since 2018, environmental standards regarding PM have become more stringent. Pulse air jet bag filters are suitable for PM under the 20㎛ and, can function regardless of size, concentration and type. Filtration velocity and shape are important factors in the operation and design of the pulse air jet bag filters however, few established studies support this theory. In this research, numerical simulations were conducted based on experimental values and, several methods were employed for minimizing the pressure drop. In the pilot system, as the inlet duct velocity was faster than 19 m/sec, flow was not distributed equally and, re-entrainment occurred due to the hopper directional vortex. The multi-inlet system decelerated the hopper directional vortex by 25 ~ 30% , thereby decreasing total pressure drop by 6.6 ~ 14.7%. The guide vane system blocked the hopper directional vortex, which resulted optimal vane angle of 53°. The total pressure of the guide vane system increased by 0.5 ~ 3% at 1.5 m/min conditions. However, the filtration pressure drop decreased by 4.8 ~ 12.3% in all conditions, thereby reducing the operating cost of filter bags.