• Journal of the Korea institute for structural maintenance and inspection
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• v.20 no.6
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• pp.98-105
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• 2016

In this study, projectiles with 2 kinds of nose shape: spherical and flat were impacted into normal concrete and fiber reinforced concrete panels. The fracture depth and form, crater diameter, tensile strain at rear face were evaluated. It was confirmed that smaller projectile nose areas resulted in deeper penetrations associated with concentrated impact forces and small front-face crater diameters in impact test. Conversely, larger projectile nose areas resulted in shallower penetrations and larger front-face fracture diameters. Similar front-face failure and strain distribution relationships based on the projectile nose shape were observed for normal and fiber-reinforced concrete although the rear-face tensile strain and scabbing were significantly reduced by the fiber reinforcement. In addition, a direct relationship was confirmed between the penetration depth based on the projectile nose shape and the tensile strain on the rear face. Thus the impact strain behavior is required to predict the scabbing behavior with penetration depth.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.3
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• pp.1-7
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• 2002

An experimental study was conducted to investigate the effects of leading edge extension(LEX) on the surface prssure distribution over a delta wing in a subsonic wind tunnel. Freestream velocity was 40m/sec and Reynolds number per meter was 1.7x$10^6$ with total pressure of 101Pa and total temperature of 278K. LEX changed the surface pressure distribution on the wing dramatically. Comparing with the results without LEX, the peak of pressure distribution decreased on the front chordwise location but it turned to increase on the rear chordwise location with increase of the angle of attaci. The spanwise gradient of the pressure distribution also increased in the rear chordwise location. Without LEX, the peak of pressure distribution increased and decreased irregularly with increase of the angle of attack at each chordwise location, but LEX made it increased almost linearly with increase of the angle of attack at all of the chordwise locations.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.8
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• pp.735-743
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• 2011

In this study, the distribution of surface pressure was measured in a steady state on a turbine blade which was moved the injected region and receded the stagnation region using a linear cascade apparatus. Axial-type blades were used and the blade chord was 200mm. The rectangular nozzle was applied and its size was $200mm{\times}200mm$. The experiment was done at $3{\times}10^5$ of Reynolds number based on the chord. The surface pressures on the blade were measured at three different nozzle angles of $58^{\circ}$, $65^{\circ}$ and $72^{\circ}$ for off-design performance test. In addition, three different solidities of 1.25, 1.38 and 1.67 were applied. From the results, the low solidity caused the low pressure on the blade suction surface at entering region and the reverse rotating force was generated at the low nozzle angle. The positive incidence also made the pressure lower on the suction surface at entering region.

• Journal of Adhesion and Interface
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• v.18 no.4
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• pp.171-178
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• 2017

Recently, layer-by-layer (LbL) assembly has emerged as a promising fabrication technique in controlling surface wetting properties. LbL assembly technique is eco-friendly versatile technique to control the hierarchical structure and surface properties in nano- and micro-scale by employing a variety of materials (e.g., polymers, surfactants, nanoparticles, etc.). This article reviews recent progress in controlling the surface wetting using LbL technique. In particular, technical trends and research findings on fabrication and the applications of superhydrophobic, superhydrophilc, and superoleophobic/superhydrophilic LbL surfaces are extensively explained. Additionally, basic principles and fabrication methods in emerging areas such as omniphobic, self-healing, intelligent and responsive LbL surfaces are discussed.

• Proceedings of the Korean Vacuum Society Conference
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• 2013.02a
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• pp.301-301
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• 2013

구동형 부품(Actuated component)중의 하나인 LeadScrew는 이송장치를 구성하는 핵심 부품으로 소재로는 탄소강, 합금강, 스테인레스강 등이 주로 이용된다. 다양한 IT기기의 정밀 이송 및 고속 구동에 사용되며, 제품의 성능을 결정하는 중요 핵심 부품으로 사용되고 있다. IT기기용 구동 요소 부품은 정밀 가공성의 제약으로 내식성이 우수한 스테인레스강 소재보다는 일반적으로 소재비가 저렴하고 가공성이 우수한 탄소강 소재를 사용하게 되며, 위 소재를 사용하면 대기중의 수분등에 의한 부식환경에서 쉽게 부식되어 부식방지를 위한 표면처리 기술개발이 필요하다.또한, 구동형 부품은 부품 상호간의 심한 마찰 등과 같은 가혹한 조건에 노출되어, 부품의 내마모성 및 표면 경도등을 향상시켜 부품의 수명을 연장하고자 한다. 그러기 위해 선 표면경도, 내마모성, 내식성 등의 다양한 기능이 요구되며, 성능을 만족시키기 위해서 열표면처리 공정을 확인하고자 한다.본 연구에서는 냉간압조용 강선인 SWCH계열 표면에 PECVD 장치로 플라즈마 질화공정을 이용하여 동일조건(압력, Gas flow, Power)하에서 $500{\sim}550^{\circ}C$의 온도 범위 내에서 30~300 min의 시간 조건으로 실험을 진행하였다. 위 시험편으로 XRD를 통해 각 플라즈마 질화 공정 조건에 따른 상 변화를 확인하였고, 염수분무테스트를 통해 내식성을 확인하였다. 표면경도 및 단면경도를 통한 실용질화층을 확인하고, 마모테스트를 통하여 마찰계수를 확인하여 표면경도, 내마모성, 내식성을 충족하는 공정에 대한 실험을 진행하였다.

• Korean Journal of Materials Research
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• v.8 no.9
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• pp.825-830
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• 1998

자화된 유도결합형 C4F8 플라즈마로 SiO2를 건식식각시 실리콘 표면에 발생하는 손상과 오염에 대하여 연구하였다. 오염의 분석을 위해서 XPS, SIMS, TEM을 사용하였으며, 손상정도를 측정하기 위해서 HRTEM과 Schottky-diode 구성을 통한 I-V특성 측정을 사용하였다. 유도 결합형 C4F8 플라스마에 0에서 18Gauss까지의 자장이 가해짐에 따라서 실리콘 표면에 생기는 잔류막의 두께가 SiO2식각속도와 선택비의 증가와 함께 증가하였으며, XPS를 통하여 그 조성이 fluorine-rich에서 carbon-rich 한 상태로 변화함을 알 수 있었다. 자장을 가하지 않는 상태에서는 표면에서 $40\AA$부근까지 고밀도의 손상층이 관찰되었으나, 자장을 가함에 따라서 노출된 손상층의 깊이는 깊어지나 그 밀도는 줄어들음을 HRTEM을 통하여 관찰 할 수 있었다. Schottky-diode를 통한 I-V특성곡선의 분석으로 자장이 증가함에 따라서 전기적인 손상이 감소함을 알 수 있었다.

• Polymer Science and Technology
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• v.19 no.5
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• pp.406-409
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• 2008

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2002.05a
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• pp.31-31
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• 2002

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2000.05a
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• pp.6-6
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• 2000

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2000.05a
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• pp.36-36
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• 2000