• 한국추진공학회지
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• 제9권4호
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• pp.39-47
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• 2005

재생냉각형 액체로켓 연소기 챔버 냉각 채널부의 상온상태의 구조해석과 검증시험을 수행하였다. 재생냉각 연소기 냉각 채널부에 사용하는 구리 합금의 상온 인장시험을 수행하여 재료의 탄소성 물성 값을 확보하였으며 냉각 채널의 탄-소성해석은 이 물성 값을 이용하여 수행하였다. 해석결과의 검증을 위해서 평판형태의 냉각채널 시편을 제작하여 강도시험을 수행하였다. 탄-소성 구조해석 결과와 시편의 수압시험 결과 사이에 약간의 차이는 있지만 비교적 잘 일치하였으며 채널의 단면 두께가 작기 때문에 제작상의 가공오차가 채널의 구조적인 안정성에 큰 영향을 미치는 것을 확인하였다.

• 한국전자파학회논문지
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• 제13권2호
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• pp.188-195
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• 2002

본 논문에서는 GTEM 셀을 이용하여 복사장을 예측하는 알고리즘 중 대표적인 두 가지 기법인 3 방위와 15방위 기법에 대해 전자파 반-무반사실에서 측정한 결과와의 상관관계를 통계적으로 검증하였다. 그리고 이론적인 다이폴 모델에 대해 이 두 가지 기법을 적용하여 접지면상의 복사장을 구하고 그 값을 이론치와 비교하였다. 두 알고리즘을 이용한 견과와 전자파 반-무반사실 측정 결과는 상관계수가 모두 0.8 이상으로 높은 상관성을 가짐을 확인할 수 있고, 기존 3 방위 기법에 의해 계산된 값은 전자파 반-무반사실 혹은 15 방위 기법보다 높게 계산됨을 이들 결과로부터 알 수 있었다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제34회 춘계학술대회논문집
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• pp.321-325
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• 2010

Supersonic ejectors are simple mechanical components, which generally perform mixing and/or recompression of two fluid streams. Ejectors have found many applications in engineering. In aerospace engineering, they are used for altitude testing of a propulsion system by reducing the pressure of a test chamber. It is composed of three major sections: a vacuum test chamber, a propulsive nozzle, and a supersonic exhaust diffuser. This paper aims at the improvement of ejector-diffuser performance by focusing attention on reducing exhaust back flow into the test chamber, since alteration of the backflow or recirculation pattern appears as one of the potential means of significantly improving low supersonic ejector-diffuser performance. The simplest backflow-reduction device was an orifice plate at the duct inlet, which would pass the jet and entrained fluid but impede the movement of fluid upstream along the wall. Results clearly showed that the performance of ejector-diffuser system was improved for certain a range of system pressure ratios, whereas the orifice plate was detrimental to the ejector performance for higher pressure ratios. It is also found that there is no change in the performance of diffuser with orifice at its inlet, in terms of its pressure recovery. Hence an appropriately sized orifice system should produce considerable improvement in the ejector-diffuser performance in the intended range of pressure ratios.

• 한국군사과학기술학회지
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• 제7권4호
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• pp.133-137
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• 2004

A simplified test rig to simulate high-altitude environments was designed by analyzing the AEDC (Arnolds Engineering Development Center) report regarding simulated altitude testing. The test rig consists of a vacuum chamber, a supersonic nozzle connected to a cold-gas supplier and a diffuser. The preliminary tests were conducted to validate the AEDC design concepts. The test results showed that sub-atmospheric pressure(1.0psia) environments were realized inside the vacuum chamber and the design concepts were confirmed.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 제33회 추계학술대회논문집
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• pp.403-406
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• 2009

본 연구는 MIL-HDBK-310을 기준으로 한 고도별 대기상태 즉, 온도, 습도 및 압력을 모사하여 고도에 따른 피시험물의 성능을 MIL-STD-810F 및 AIAA-2466에서 정한 시험 절차에 따라 평가하는 챔버를 개발하는 것이다. 이를 위한 대기차단 구조물, 시험부 및 공기순환유로, 고도모사 배기장치, 온도제어장치, 습도제어장치 및 설비제어장치 등을 설계하는데 고려하여야 할 사항을 기술하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.105-110
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• 2010

Supersonic ejectors are simple mechanical components, which generally perform mixing and recompression of two fluid streams. Ejectors have found many applications in engineering. In aerospace engineering, they are used for high altitude testing (HAT) of a propulsion system by reducing the pressure of a test chamber. It is composed of three major sections: a vacuum test chamber, a propulsive nozzle, and a supersonic exhaust diffuser (SED). This paper aims at the improvement in HAT facility by focusing attention on the vertical firing rocket test stand with shock generators. Shock generators are mounted inside the SED for improving the pressure recovery. The results clearly showed that the performance of the ejector-diffuser system was improved with the addition of shock generators. The improvement comes in the form of reduction of the starting pressure ratio and the vertical height of test stand. It is also shown that shock generators are useful in reducing the total pressure loss in the SED.

• 한국산업보건학회지
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• 제19권2호
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• pp.96-101
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• 2009

The purpose of this study was to conduct the field validation of alternative method(ETM method) by using non-carcinogenic, and less toxic solvents than NIOSH (National Institute for Occupational Safety and Health) analytical method 5524 for measuring the airborne metalworking fluids in workplaces. We carried out the field validation test by using the exposure chamber, guaranteeing the air sampling homogeneously in a machining environment. The ETM mixed solvent presented the complete solubility of MWFs used in test field. Based on the field test data, the bias of the ETM method from reference method, NIOSH analytical method 5524, was from -7.0% to 5.1%. The overall uncertainty of the ETM nethod was 21.6%, which satisfied the NIOSH criteria for the sampling and analytical criteria.

• 한국철도학회논문집
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• 제9권4호
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• pp.349-356
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• 2006

At present, the selecting system and analytic estimation criterion on repair materials and methods of the deteriorated RC structures have not yet been set up in domestic. Under these circumstances, deterioration such as shrinkage crack, corrosion of rebar has been often occurred after repair, and this finally results in too frequent repairs. In this study, three types of repair methods were experimentally investigated by the accelerating test in a combined deterioration chamber and long-term field exposure test. Three types of repair methods applied in this study belong to a group of polymer cement mortar, which is commonly used in repair works. According to the results of this study, durability of repair mortar layers and corrosion properties of recovered rebar could be investigated in short period by the accelerating test in a combined deterioration chamber, which can simulate the condition of repeated high-and-low temperature and repeated dry-and-wet environment, spraying chloride solution and emitting $CO_2$ gas. After 36 month long-term filed exposure test in the coastal area, harmful macro-cracks are observed in the polymer cement mortar layer of some repair methods. These crack are considered to result from drying shrinkage of polymer cement mortar. Also, after 36 month exposure, amount of corrosion area and weight loss of rebar are found to be different according to the types of repair methods.

• 대한전자공학회논문지TC
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• 제47권4호
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• pp.18-24
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• 2010

본 논문은 전자파장해 및 복사 내성 측정에 사용되는 전자파 무반사실의 대용 방법으로 사용되는 전자파 잔향실 내의 필드 균일성에 관한 연구이다. 최근 Wireless LAN 이나 DMB 및 휴대 인터넷 사용량의 증가로 인해 전자기파 노이즈가 다른 기기나 장비에 악영향을 미칠 것으로 예상되는 2.3 GHz 대역에 초점을 맞추었다. 본 논문에서는 전자파 잔향실 내부의 전계강도 수치해석을 위하여 시간영역 유한 차분법이 사용되었으며, 전자파 잔향실의 특성과 내부 전계강도의 균일성 개선을 위하여 2D CRD의 배치와 개수를 변화시키면서 표준 편차, 공차 특성, 편파 특성을 비교분석하였다. 전자파 잔향실의 두 면에 확산기를 부착하였을 때 확산기를 사용하지 않은 전자파 잔향실에 비하여 표준 편차는 1.98 dB, 공차 특성은 3.6 dB 만큼 개선되었다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2000년도 제14회 학술강연논문집
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• pp.8-8
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• 2000

In this paper are presented main power and gasdynamic characteristics of C-l6VK hypersonic test cell of Research Test Center of CIAM. Gasdynamic adjustment of the C-l6VK test cell was carried out with the working section constructed on scheme of Ramjet/scramjet test in free stream. Gasdynamic adjustment was conducted stage by stage in tile following sequence. First, check and preparation of all technical systems and checking measuring system. Than determination of the characteristics of test cell on cold (without the heating of air at entrance) regime and determination of the characteristics of test cell on regimes with the heating of air. Finally determination of tile characteristics of test cell with the loading of the working part by object. On tile final stage of gasdynamic adjustment two experiments with tile axisymmetric Scramjet model loaded into the working part of test cell were conducted. The first experiment was conducted with the purpose of determination of flow parameters with the object leaded into the working part and verification of experiment cyclogram. The second experiment was conducted with injection of hydrogen into the combustion chamber of object, that is tile conditions on test cell simulated Scramjet flight Mach number M = 6. Such methodology of gasdynamic adjustment allows to determine influence of experimental object on flow parameters in the working part at different conditions of experiment (with the burning in combustion chamber of object and without the homing), and also to compare flow characteristics in the object duct.