• Journal of the Korean Society for Nondestructive Testing
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• v.33 no.4
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• pp.388-393
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• 2013

• Proceedings of the Korean Vacuum Society Conference
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• 1997.02a
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• pp.110-111
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• 1997

• Computational Structural Engineering
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• v.16 no.2
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• pp.62-70
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• 2003

• The Monthly Technology and Standards
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• s.1
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• pp.54-58
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• 2002

• Composites Research
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• v.31 no.5
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• pp.260-266
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• 2018

This study investigates thermal and mechanical characterization of Hafnium carbide coating on the $C_f-C$ composites. The hafnium carbide coatings by vacuum plasma spray on the C/C-SiC composites are prepared to evaluate oxidation and wear resistance. We perform the thermal durability tests by thermal cycling at $1200^{\circ}C$ for 10cycles in air and investigates the weight change of each cycle. We also evaluate the wear and indentation behavior using tungsten carbide ball indenter as a mechanical evaluation. As a result, the HfC coating is beneficial to reduce of weight loss during thermal cycling test and improve the elastic property of C/C-SiC composite. Especially, the HfC coating improves the wear resistance of C/C-SiC composite.

• Journal of the Korean Society for Precision Engineering
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• v.26 no.2
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• pp.21-25
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• 2009

• Proceedings of the KWS Conference
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• 2002.05a
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• pp.211-213
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• 2002

• Korean Journal of Materials Research
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• v.5 no.3
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• pp.310-315
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• 1995

기계적으로 연마한 고속도강과 구리 두 종류의 서로 다른 기판상에 dc 마그네트론 스파터법으로 TiN 박막을 성막시켜 코팅층의 비커스 미소경도를 측정하였다. 압입체의 침투깊이와 시험하중과의 관계를 log-log 좌표상에 도시함으로써 기판의 영햐응ㄹ 받지 않고 코팅층만의 경도를 측정할수 있는 최대하중인 임계하중(critical load)을 구할수 있었다. 임계하중을 가했을 때 압입체의 침투깊이와 코팅층 두께간의 비율은 코팅층의 두께에 무관하였고 기판의 경도에 크게 의존하였다.

• Journal of the Korean Society of Manufacturing Process Engineers
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• v.17 no.5
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• pp.8-15
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• 2018

Films with special properties (e.g., water-repellent films, optical films, anti-reflection films, and flexible films) are referred to as functional films. Recently, there has been interest in fine patterning methods for film fabrication. In particular there have been many studies that use a UV nanoimprint process involving a UV curing method. In this paper, a polymer film was fabricated by the UV nanoimprint process with a micro-pattern, and its durability was evaluated by a wear test and a nano-indentation test. The film mechanical properties (such as coefficient of friction, hardness, and modulus of elasticity) were measured. Moreover, the choice of PUA type resin used in the UV nanoimprint process was confirmed to impact the durability of the thin film. Despite making the polymer film samples using the same method and PUA type resin, different coefficient of friction, hardness, and modulus of elasticity values were obtained. PUA 4 resin had the most favorable coefficient of friction, hardness, and modulus of elasticity. This material is predicted to produce a high durability functional film.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.47 no.1
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• pp.26-34
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• 2019

In this paper, a coarse lunar soil model is developed using discrete element method and its computed physical properties are compared with those of the actual lunar soil for its validation. The surface of the actual moon consists of numerous craters and rocks of various sizes, and it is covered with fine dry soil which seriously affects the landing stability of the lunar lander. Therefore, in consideration of the environment of the lunar regolith, the lunar soil is realized using discrete element method. To validate the coarse model of lunar soil, the simulations of the indentation test and the direct shear test are performed to check the physical properties(indentation depth, cohesion stress, internal friction angle). To examine the performance of the proposed model, the drop simulation of finite element model of single-leg landing gear is performed on proposed soil models with different particle diameters. The impact load delivered to the strut of the lander is compared to test results.