• Aerospace Engineering and Technology
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• v.2 no.2
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• pp.105-114
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• 2003

It is conducted to analyze vibration loads on the 1st stage of KSR-III(KSR : Korea Sounding Rocket) during their ground transportation and various handling process. These loads may be different from the real flight environment. Inadequate assessment of these loads can cause not only local damages on the rocket system but also the critical problem like flight mission failure. Therefore, transportation and handling loads must be considered during design and attenuated to ensure that the rocket structural damage does not occur. This work is concerned with the generation of criteria and prediction of transportation and handling loads for KSR-III. The results show that the shipping container is well designed to satisfy the design requirements. The maximum vibration level recorded during whole transportation and handling for KSR-III is less than 2g, the criteria of KSR-III movement condition.

• Korean Chemical Engineering Research
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• v.47 no.3
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• pp.321-326
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• 2009

A simple measuring device is proposed, and its performance is examined in an adsorption process separating a gas mixture. The sensor is made of a quartz crystal resonator and solid adsorbent to detect the target component. Micro-particle carbon cryogel(MCC) is utilized as the adsorbent, and the gas mixture of air and i-butane are separated in a column containing bamboo activated carbon. Two devices are placed at the inlet and outlet of the column. The measurements are compared with those of GC outcome to prove the measurements are effective. The experimentally proved system is simple and capable to be implemented in an in-line system with on-line measurement.

• Journal of Aerospace System Engineering
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• v.14 no.spc
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• pp.39-48
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• 2020

This paper deals with the process of estimating the environmental noise generated from the actual flying aircraft using the noise measurement results obtained through the wind tunnel test and verifying it through flight tests. In order to evaluate the environmental noise of an aircraft, noise tests and evaluations are generally conducted according to the procedures prescribed by the International Civil Aviation Organization (ICAO). In this paper, we introduced environmental noise evaluation method that can be applied to composite both fixed-wing aircraft and multi-copter, and introduced the evaluation method by experiment. This paper introduces the process of simulating the noise test results measured in the wind tunnel test using real flight test results. In addition, in consideration of flight operating conditions and noise measurement methods proposed by the ICAO, the effective perceived noise level (EPNL) was predicted by performing both the wind tunnel test and the aircraft flight test.

• Membrane Journal
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• v.33 no.6
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• pp.447-453
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• 2023

The performance of computer systems and the development of various computer simulation programs have made it possible to analyze chemical systems composed of more complex elements, and accordingly, research using molecular dynamics simulation is being actively conducted. Research on calculating the gas permeation characteristics of polymer membranes by molecular dynamics, which was previously conducted mainly through experiments, is receiving attention for gas barrier membranes used in food packaging and pharmaceuticals. Recently, there has been a report that a gas barrier effect appears when a coating film is made using silk fibroin, and in this study, a study was conducted using molecular dynamics simulation to confirm whether an oxygen barrier effect appears when a composite film is made using silk fibroin. We built a single model, calculated the gas permeation characteristics, and compared it with the experimental value to confirm that the model reflects the actual experimental results. Actual composite membrane models were then built and the gas movement path within the polymer was analyzed. As a result, oxygen molecules were found that they could not pass through and was blocked in the fibroin region. Therefore, the composite membrane with silk fibroin has excellent oxygen barrier property and is expected to be useful in food packaging, etc.

• Journal of the Korean Society of Propulsion Engineers
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• v.20 no.3
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• pp.17-24
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• 2016

The reacting flows of gaseous hydrogen/liquid oxygen 2D coaxial shear injector with varying recess length are numerically analyzed. The standard ${\kappa}-e$ model and laminar flamelet model are adopted for the steady turbulent combustion with the ideal and real gas equations. As the recess length increases, the recirculating region in the combustion chamber expands and the vorticity is intensified. Also, the variations of temperature, products, and pressure are strongly related to the recess length. The results show that an efficient combustor can be obtained by the introduction of the recessed injector.

• 한국신재생에너지학회:학술대회논문집
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• 2007.11a
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• pp.221-223
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• 2007

고분자전해질연료전지의 효율과 수명은 고분자 전해질 막과 밀접하게 관련되어있다. 연료전지 상용화를 위해 내구성과 안정성은 반드시 확보되어야 한다. 본 연구에서는 고분자전해질연료전지용 막전극접합체에 대해서 제작과정, 체결과정 및 운전 중에 발생할 수 있는 물리적 손상이 연료전지에 미치는 영향을 알아보고자 하였다. 실제 고분자전해질연료전지 조건에서 구멍이 생기는 경우를 모사하기 위해 막전극접합체에 다양한 크기 및 형상의 물리적 손상을 형성시켰다. 또한 여러 위치에서의 손상도 비교하였다. 손상시킨 막전극접합체에 대해 단위전지 성능평가와 순환전압전류 실험을 비교 분석하였다. 막전극접합체의 결함이 커질수록 수소기체투과도는 증가하고, OCV와 성능은 감소하였다. 또한 성능과 수소기체투과도는 서로 관련이 있음을 알 수 있었다.

• Proceedings of the Korean Vacuum Society Conference
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• 2010.08a
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• pp.40-40
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• 2010

사중극 질량 분석기(Quadrupole Mass Spectrometer, QMS)는 높은 정확도와 사용이 쉬운 장점으로 인해 반도체 및 디스플레이 산업 등의 진공공정에서 잔류가스를 측정하고 분석하는 기기로써 반도체 및 디스플레이 소자제조를 위한 공정 진단에서 많이 사용되고 있다. 특히 고진공으로 내려가면서 리크 디텍션(leak detection)과 미세 량의 잔류기체 감지가 더욱더 요구되며 특히 $H_2$ 및 CO의 경우 측정에 많은 어려움이 있다. 따라서 $H_2$ 및 CO의 미세 량을 감지하기 위하여 QMS의 성능을 평가할 수 있는 parameter 중 하나가 될 수 있는 minimum detectable partial pressure(MDPP)를 측정하였다. 실제 고진공에 도달하여 MDPP를 계산하기 위해서는 bake out이 필요하며 또한 가스가 주입되지 않은 상태에서 잔류기체의 조성을 정확히 알 수 없기 때문에 정량적 분석이 어렵다는 단점이 있다. 본 실험에서는 측정하고자 하는 물질의 소량 포함된 표준가스를 사용하여 부피확장방법으로 가스 챔버로 희석하여 이동시키고 핀홀에서 가스유량을 더 줄여서 QMS가 기체를 감지하는 압력범위를 유지하면서 가스를 인가하여 주어 그때의 MDPP를 계산하였다. 또한 tuning을 통해 이온전류를 증폭시켜 더 향상된 MDPP를 측정하였다. 이 방법을 사용하면 bake out을 통한 고진공에 도달하지 않고서도 MDPP를 측정할 수 있으며, 정확한 조성 및 부분압을 알 수 있고 또한 희석된 가스를 사용하여 MDPP를 더욱 더 향상시킬 수 있다.

• Bulletin of Food Technology
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• v.13 no.2
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• pp.3-13
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• 2000

신선 과일, 채소 편의식품의 주요 특징으로는 박피, 절단 등에 의한 식물조직의 손상, 최소가공에 따른 제품의 불확실한 미생물 안전성, 식물 조직의 활발한 물질대사, 제품 종류의 제한 등을 들 수 있다. 따라서 이들 제품에서는 미생물이 증식하기 쉬우나 실제 미생물의 거동은 식물조직의 대사에 의해 영향을 받으며, 또한 생체의 호흡과 필름 포장재의 기체투과도에 의해 좌우되는 포장내부 환경기체에도 영향을 받는다. 수확후 감염은 과일, 채소와같은 원료 농산물의 주요 손실요인으로(Harvey, 1978;Lund, 1983) 신선 과채류 편의식품의 경우 절단면의 노출과 포장내부의 고수분 함량 등에 의해 미생물 감염의 위험은 더욱 더 증가할 수 있다. 특히 대부분의 신선 편의식품이 어떠한 가열처리도 없이 그대로 이용되므로 식품유래 병원균의 오염과 저장중 이들의 증식은 각별한 관심의 대상이 되고 있다. 이에 본고에서는 현재 과채류 편의식품에 주로 사용되고 있는 미생물 오염 방지 또는 조절 방법에대해 설명하고 이의 적용과 관련한 주의사항을 살펴보고자 한다.

• 한국전산유체공학회:학술대회논문집
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• 2005.10a
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• pp.187-194
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• 2005

For the analysis of compressible multi-phase and real gas flows, characteristic form of Roe's Riemann solver was derived using real gas equation of state. It was extended to multi component reactive system considering variable specific heat. From this study, it is known that some correction should be made for the use of existing numerical algorithm. 1) Sonic speed and characteristic variable should be corrected with real gas effect. 2) Roe's average was applicable only with the assumption of constant properties. 3) Artificial damping term and characteristic variables should be corrected but their influences may not be significant.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.8 no.2
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• pp.279-287
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• 1996

A cycle analysis is performed to investigate how the non-ideal gas behavior of helium reduces the heating capacity of VM heat pumps. Since the operating pressures of VM heat pumps are as high as 1 to 20 MPa, the compressibility factor of helium becomes clearly greater than 1 and the non-ideal behavior always represents a thermal loss in heating. To calculate the amount of the losses, an adiabatic cycle analysis is performed with the real properties of helium and the net enthaply flows through the two regenerators are numerically obtained. It is shown that the non-ideal gas losses could be as much as 8% in the heating capacity when the operating pressures are greater than 10MPa. The effects of the operating temperatures and the dead volumes on the loss are presented.