• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2004년도 추계 학술대회논문집
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• pp.95-99
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• 2004

The developing Smart UAV in KARI supposes high speed flight as like a conventional plane, as well as vertical takeoff and landing as like a helicopter. Therefore, the air intake system should be designed to provide the sufficient air flow to the engine and the maximum possible total pressure recovery at the engine intake screen over a wide range of flight conditions. For this purpose, we designed the intake system using a pilot type intake model and plenum chamber In this paper, we designed the intake model and analyzed the performance of designed intake system using the general-purpose commercial CFD code, CFD-ACE+ For 3-D calculation, we generated mesh using the unstructured gird and used $\kappa-\epsilon$ turbulence model. The analysis results of the total pressure variation and the velocity distribution was illustrated in this paper. The pressure recovery and distortion coefficient at a plane coincident with the compressor inlet were calculated and streamline variation through the intake system was investigated at the worst condition as well as the standard flight condition.

• 한국항공우주학회지
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• 제45권12호
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• pp.1031-1038
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• 2017

공기 흡입식 엔진의 성능 향상을 위하여 흡입구를 통한 유입공기의 전압력 회복률을 최대로 하는 것은 엔진 설계에 있어서 매우 중요하다. 흡입구의 각 램프 단에서 발생하는 충격파의 세기를 동일하게 흡입공기를 압축하면 흡입구에서의 최대 전압력 회복을 보장한다는 Oswatitsch 기법이 극초음속에서도 유효한지를 조사하였다. 극초음속 영역에서의 흡입구 작동 한계를 고려하여 압축 특성 및 열역학적 관점에서 유입 마하수에 따른 흡입구의 압축램프 각도와 램프 수에 따른 흡입구 성능을 비교하여 각단에서 발생하는 충격파 강도에 영향을 주는 경사 충격파에 수직한 마하수의 비선형성을 분석하였다. 이 분석을 근거로 Oswaitisch 기법이 초음속에서 뿐만 아니라 극초음속 비행 영역에서도 유효한 결과를 도출할 수 있음을 확인하였다.

• 한국항공우주학회지
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• 제37권1호
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• pp.69-75
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• 2009

본 논문은 새로운 개념의 초음속 혼합기인 벤트 혼합기의 형상적 특성에 따른 공력 특성을 연구하였다. 홀의 크기는 2 mm이며 혼합기 벽면에서 2 mm 떨어진 곳에 위치한 모델(case 1)과 혼합기 벽면 뒤쪽에 위치한 모델(case 2)의 경우 같은 전압력 회복율을 보였으며, 홀의 크기를 반으로 줄인 1 mm(case 3) 모델은 cases 1, 2에 비해 낮은 전압력 회복율을 보였다. 재순환 영역의 크기는 cases 1-3은 같지만 전단층 두께는 cases 1, 2가 case 3 보다 두꺼웠다. 재순환 영역 내 압력 손실의 경우 cases 1, 2은 case 3에 비해 낮은 압력 손실과 높은 속도 구배를 보였으며, 이는 재순환 영역 내 공기와 연료의 혼합을 증대시키는 요인이다. 재순환 영역 내로 유입 되는 유동에 의해 형성되는 박리 버블은 연소기의 전압력 회복율과 재순환 영역 내 압력 분포와 순환 유동에 영향을 미친다. 따라서 박리 버블 형성에 영향을 주는 유입 공기 유량이 벤트 혼합기 성능에 주요한 영향을 미치는 것을 알 수 있다.

• 설비공학논문집
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• 제23권4호
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• pp.281-286
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• 2011

The objective of this study is to optimize the four-bed six-step pressure swing adsorption(PSA) process for high purity $CH_4$ recovery from the biogas. The effects of P/F(purge to feed) ratio and cycle time on the process performance were evaluated. The cyclic steady-states of PSA process were reached after 12 cycles. The purity and recovery rate of product gas, pressure and temperature changes were constant as the cycle repeated. It was shown that the P/F ratio gave significant effect on the product recovery rate by increasing the amount of purge gas in purge and regeneration step. The optimal P/F ratio was found to be 0.08. As the cycle time increased, the product purity decreased by increasing the feed gas flow rate. It was found that the optimal operating conditions were P/F ratio of 0.08 and total cycle time of 1,440 seconds with the purity of 97%.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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• pp.245-250
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• 2003

In order to control indoor air quality and save energy, it is needed to install a suitable ventilation system equipped with heat exchanger for heat recovery. The purpose of this research is to find the performance of paper heat exchanger for exhaust heat recovery, which exchanges latent heat as well as sensible heat. Experimental apparatus comprises heat exchanger model, constant temperature and humidity chamber, fan and measurement systems for temperature, pressure and flow rate. Thermal performance and pressure loss of the paper heat exchanger are measured and compared at various air velocities and outdoor conditions. Experimental results show that paper heat exchanger can recover $50{\sim}70%$ of the enthalpy difference between supply and exhaust air.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.480-485
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• 2008

In this study, two types of ramjet intake were designed for the flight condition of Mach number 2 and 5 and numerical analysis was performed. In order to widen the flight envelope range(Mach number $2{\sim}6$), movable intake concept was applied. The central body was designed so that the capture area ratio which is one of most important factors of ramjet intake design could be adjusted. And various types of cowl and movable insert part of shell were designed in order to control throat area which could increase total pressure recovery. The numerical results showed that the designed ramjet intake could be applied in various flights Mach number.

• 한국농공학회:학술대회논문집
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• 한국농공학회 2000년도 학술발표회 발표논문집
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• pp.333-339
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• 2000

This study was performed to investigate the performance of heat recovery device attached to exhaust gas funnel connected to combustion chamber of greenhouse heating system. The experiment heat recovery system is mainly consisted of LPG combustion chamber and two heat recovery units; unit-A is attached directly to the exhaust gas funnel, and unit-B is connected with unit-A. Heat recovery performance was evaluated by estimating total energy amount by using enthalpy difference between two measurement points together with mass flow rate of gas and/or air passing through each heat recovery unit depending on 5 different flow rates controlled by voltage meter. The results of this experimental study, such as heat exchange behavior of supply air pipes and exhaust air passages crossing the pipes, pressure drop between inlet and outlet, heat recovery performance of exchange unit, etc., will be used as fundamental data for designing optimum heat recovery device to be used for fuel saving purpose by reducing heat loss amounts mostly wasted outside of greenhouse through funnels.

• 한국추진공학회지
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• 제6권2호
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• pp.65-74
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• 2002

전압력 회복율을 최대로 하기 위한 IRR형 램젯 공기 흡입구 초음속 확산부의 최적형상 설계를 수행하였다. 질량유량을 제약조건으로 고려하고 외부램프에서의 두 번째 경사충격파와 카울립 형상, 그리고 흡입구 목의 단면적을 설계변수로 선택하였다. 효율적인 최적화를 위해 설계변수 변환을 통한 개선된 반응면 기법을 사용하였으며 설계반복을 통해 높은 신뢰도의 반응면을 구성할 수 있었다. 최적화 기법으로 유전자 알고리즘을 사용하였으며, 이차원 Euler Code를 사용하여 공력해석을 수행하였다. 배압조건의 적용을 위해 흡입구 목 뒤로 가상의 노즐을 장착하였고 총 20회의 계산으로 종말충격파 이후의 전압력 회복율이 기준형상에 비하여 14% 향상된 초음속 확산부 최적형상을 설계할 수 있었다.

• 한국수정란이식학회지
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• 제15권3호
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• pp.279-286
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• 2000

This study was conducted to develop an improved method for oocyte pick-up(OPU) with finger-sensibility using ultrasound-guidance from ovarian follicles in Holstein heifers. Oocytes were aspirated from ovarian follicles of clear-outline (>2mm), obscure-outline and invisible($\leq$ 2mm) on ultrasound images with 3 different vacuum pressure(40, 80, 120mmHg). Total number of oocytes recovered/follicles were 309/237(130.4%). 113/80(141.3%) and 107/74(144.6%) with 40, 80 and 120 mmHg of vacuum pressure, respectively. Mean number of oocytes recovered was higher in 2 OPU/week (18.3$\pm$5.3) than 1 OPU/week(14.5$\pm$4.1), but this difference was not statistical1y significant. The recovery rates were not affected by the number of OPU as 135.6%(282 oocytes/208 follicles) in 1~20 OPU, 137.7% (168/122) in 21~40 OPU and 148.4%(92/62) in 41~60 OPU, respectively. The proportions of good oocytes (Grades I) recovered were not significantly different by the number of OPU until 40 OPU(12.4% in 1~20 OPU vs 16.7% in 21~40 OPU). However, a significantly(P<0.05) lower recovery rate resulted from more than 40 OPU compared to less than 40 OPU(7.6%). These results imply that more fertilizable oocytes can be produced from invisible-immature follicles by transvaginal aspiration with finger-sensibility from Holstein heifers.

• 설비공학논문집
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• 제17권10호
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• pp.956-964
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• 2005

In order to control indoor air quality and save energy, it is needed to install a suitable ventilation system equipped with heat exchanger for heat recovery The purpose of this research is to find the factors affecting the performance of paper heat exchanger for exhaust heat recovery, which can be applied directly to the conventional ventilation unit, air-purifier, and air-conditioning system. In this study, thermal performance and pressure loss of the paper heat exchanger are measured and compared at various operating conditions. The effectiveness of sensible, latent and total heat at the face velocity of 0.75 m/s are $77\%,\;47\%\;and\;57\%$ in the cooling condition and $77\%,\;59\%,\;and\;\%$ in the heating condition, respectively. The effectiveness for sensible heat is only affected by velocity. On the other hand, the effectiveness for latent heat is affected. by temperature and relative humidity.