• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.34 no.1
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• pp.49-59
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• 2005

• The Proceeding of the Korean Institute of Electromagnetic Engineering and Science
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• v.17 no.1 s.57
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• pp.65-70
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• 2006

• Analytical Science and Technology
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• v.20 no.4
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• pp.261-267
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• 2007

The 20 L small chamber test method is to evaluate pollutants such as TVOC, formaldehyde emitted from building materials. This method was only designed to evaluate the surface emission of sample exposed in the chamber. In this method, building materials cut with a fixed standard size are fixed in a sample sealing box. The sample sealing box is put into the 20 L test chamber. This chamber is ventilated at a standard air change rate with purified air for 7 days then the sample from the chamber is collected and analyzed to measure the emission rate of TVOC and formaldehyde. In this method, however, if the sealing box does not guarantee airtightness, accurate evaluation for the building materials can not be achieved due to the pollutants emitted from edge of the sample so called, edge effect. This edge effect can be much greater when evaluating panels such as plywood, flooring due to their surface treatment. In this study, flooring was tested to check airtightness of the sample sealing box with analytic results between 1L and 20 L test chamber. Furniture materials like LPM coated one side surface treatment and MDF coated both sides surface treatment with LPM were tested to identify whether the improvement of the sample sealing box airtightness is possible with the comparison between existing and improved test method that low VOC emission tape was used to seal the sample edge. After 7 days, MDF TVOC emission rate was different according to the existence and nonexistence of tape. The emission rate of the existing test method was $0.009mg/m^2h$ and that of improved test method was $0.003mg/m^2h$. Relative standard deviation for the existing test method was $0.004mg/m^2h$ and relative standard deviation for the improved test method was $0.002mg/m^2h$ when the same sample was analyzed three times. The improved test method in this study using low VOC emission tape was effective and able to reduce the heterogeneous effect of the edge from the sample sealing box.

• Aerospace Engineering and Technology
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• v.9 no.2
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• pp.90-97
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• 2010

A study about the fatigue life of copper alloy which is used in inner jacket of regenerative cooling chamber of liquid rocket engine has been performed. Mechanical properties of the material and fatigue life have been taken from tensile tests and low-cycle fatigue tests at room temperature and several elevated temperatures. Original universal slopes method, modified universal slopes method, Mitchell's method, Baumel and Seeger's method, and Ong's method have been used for predicting the fatigue data. It was found that the novel life prediction method should be developed for the copper alloys since almost all data have not been predicted well with the widely used methods.

• Journal of Korean Society of Environmental Engineers
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• v.32 no.4
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• pp.393-398
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• 2010

This study prepared and utilized an imitation trial test chamber for a petroleum spill to predict the concentration of discharged Volatile Organic Compounds in the air at the time of Tae-An peninsula's petroleum spill, which happened in December, 2007. The petroleum spill imitation trial test chamber measured and analyzed the concentration variation of total VOCs. As the ambient air velocity increased, so the concentration of VOCs decreased; and as the water temperature rose, the concentration of VOCs increased. Furthermore, it appears that total concentration of VOCs decrease by more than 90% 6 days after the initial petroleum spill compared to the initial concentration of VOCs.

• Proceedings of the Korea Air Pollution Research Association Conference
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• 2003.05b
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• pp.171-173
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• 2003

광화학스모그 챔버의 성능을 평가하기 위하여 파장별 광도시험, 광원의 NO$_2$ 광분해 상수, pure air experiment 등 성능실험을 수행하고, VOCs 종류 및 VOCs/NOx 비가 오존생성 및 입자상물질의 생성에 미치는 영향과 온도, 습도가 오존생성에 미치는 영향 등을 평가하였다. (중략)

• Proceedings of the KSME Conference
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• 2005.11a
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• pp.22.1-22.1
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• 2005

• Proceedings of the Korean Vacuum Society Conference
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• 2008.08a
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• pp.199-199
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• 2008

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.6
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• pp.526-532
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• 2015

In order to relieve limitation of flight operation under icing condition and verify its operation in adverse weather condition for Surion, military helicopter developed in Korea, airworthiness certification in icing condition is required. The process of Surion icing certification should be considered by implementation of four methods by step such as CFD analysis, simulated flight tests, artificial icing flight tests, and natural icing flight tests. For Surion icing flight tests, these are required 20~30 sorties and 20~23 hours in artificial icing condition; 20~30 sorties and 20~22 hours in natural icing condition. In addition, to proceed with efficient flight tests, it is necessary to implement artificial icing flight tests in LWC $0.5{\sim}1.0g/m^3;$ natural icing flight tests in less than LWC $0.5g/m^3$.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.11a
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• pp.403-406
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• 2009

This research is based on the altitude temperature, pressure and humidity, as defined by MIL-HDBK-310 standard and modifies this conditions to conform to the new standard MIL-STD-810F and test procedure given in AIAA-2466 from this fundamental guideline optimal design and sizing of test section, inlet, exhauster duct, temperature and humidity control was performed.