• Proceedings of the KSME Conference
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• 2003.11a
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• pp.97-102
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• 2003

An experimental study is conducted to investigate the effects of duct corrugation angle on heat/mass transfer characteristics in wavy ducts by using a naphthalene sublimation technique. The corrugation angles of the wavy ducts are $145^{\circ}$ , $130^{\circ}$ and $115^{\circ}$ . and the Reynolds numbers based on the duct hydraulic diameter vary from 300 to 3,000. At the low $Re(Re{\leq}1000)$, high heat/mass transfer regions are formed by the secondary vortex flows called Taylor-Gortler vortices on both pressure-side and suction-side walls. At the high $Re(Re{\geq}1000)$, the effects of these secondary flows are vanished. As corrugation angle decreases, the local peak Sh induced by Taylor-Gertler vortices are increased and average Sh also enhanced. More pumping power (pressure loss) is required with the smaller corrugation angle due to the stronger secondary vortex flows.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.28 no.7
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• pp.789-799
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• 2004

An experimental study is conducted to investigate the effects of duct corrugation angle on heat/mass transfer characteristics in wavy ducts of a primary surface heat exchanger application. Local heat/mass transfer coefficients on the wavy duct sidewalls are determined by using a naphthalene sublimation technique. The corrugation angles(${\alpha}$) of the wavy ducts are 145$^{\circ}$, 130$^{\circ}$, 115$^{\circ}$ and 100$^{\circ}$. And the Reynolds numbers based on the duct hydraulic diameter vary from 300 to 3,000. The results show that at the low Re(Re $\leq$1000), the secondary vortices called Taylor-Gortler vortices perpendicular to the main flow direction are generated due to effect of duct curvature. By these secondary vortices, high heat/mass transfer regions are formed on both pressure-side and suction-side walls. At the high Re(Re $\geq$ 1000), these secondary flows are vanished with helping flow transition to turbulent flow and the regions which show high heat/mass coefficients by flow reattachment are formed on suction side. As corrugation angle decreases, the local peak Sh induced by Taylor-Gortler vortices increase at Re $\leq$1000. At high Re(Re $\geq$ 1000), by the existence of different kind of secondary flows called Dean vortices, non-uniform Sh distribution appears along spanwise direction at the narrow corrugation angle (${\alpha}$=100$^{\circ}$). Average Sh also increase by the enhanced effect of secondary vortices and flow reattachment. More pumping power (pressure loss) is required with the smaller corrugation angle due to the enhancement of flow instability.

• Journal of the Korean Ceramic Society
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• v.38 no.5
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• pp.479-484
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• 2001

고순도 알루미나 분말에 소결조제로서 MgO를 0ppm 및 500ppm 첨가하여 열분무건조기를 사용하여 준비한 과립을 80$0^{\circ}C$에서 하소를 함으로써 얻어진 과립으로 제작한 소결체의 MgO 첨가량에 따른 미세구조와 꺾임강도에 미치는 영향을 고찰하였다. 또한 시편두께를 50$mu extrm{m}$의 박편으로 가공하여 투광법으로 내부구조도 관찰하였다. MgO를 500ppm 첨가하여 제작한 과립을 180 MPa의 냉간정수압성형성 후 1$600^{\circ}C$에서 소결한 소결체는 상대밀도가 100%에 도달하였고 균일한 결정립성장의 치밀한 미세구조를 나타내었다. MgO를 500ppm 첨가한 시편의 4점 꺾임강도 또한 각 소결온도에서 MgO를 9ppm 첨가한 시편보다 23%-32%정도 높은 강도를 나타내었으며, 특히 소결온도 1$600^{\circ}C$에서는 꺾임강도가 501MPa 그리고 weibull 계수가 20의 고강도이면서 신뢰성이 높은 알루미나 소결체가 얻어졌다. 본 연구에서는 weibull 계수의 값이 높은 시편일수록 내부구조의 결함크기가 작고 이 작은 결함이 시편내부에 균일하게 분포되어 있음을 확인할 수 있었다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.49 no.3
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• pp.221-231
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• 2021

In the present study, numerical simulation was performed to investigate aerodynamic characteristics of a ducted fan-upper/lower vanes system in hover. Sensitivity analysis of aerodynamic forces for a system component was conducted with the deflection angle of upper vanes varying but at the constant rotational speed and the collective pitch angle of fan blades. Then, vane control performance and duct airload distributions were analyzed in detail to physically understand operating mechanisms of individual vane and interference effect between duct and vanes. Finally, new control concept of operating upper vanes has been proposed to improve the control performance of the full configuration. It is found that the side force and rolling moment of upper vanes increase linearly with the variation of those deflection angle; however, the total side force is significantly small due to the reaction force acted on the duct. It is also found that upper vanes close to the duct contraction side have a key role in changing vane control forces. It is revealed that the duct suction pressure is induced by the interaction with the suction side of upper vanes, while duct pressure recovery by the interaction with the pressure side, leading to increase in duct asymmetric force. When four upper vanes are kept in situ at 0° deflection angle or removed, the total control performance was improved with duct asymmetric force reduced and the total magnitude of roll remarkably increasing up to 80%.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.35 no.8
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• pp.933-940
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• 2011

Thin sheets with a corrugated structure are generally used for the fabrication of heat exchangers for electronics, airplanes, and vehicles. However, it is difficult to fabricate corrugated structures, especially those with a bent angle, using the conventional stamping process because of its intrinsic formation mechanism. We propose a novel rubber-forming process for the effective pressing of the both tilted sides of a plate under the same pressure to form exact corrugated shapes. We use finite element analysis and experiments to study the rubber-forming process parameters, and we evaluate the maximum allowable bent angle for high-quality formation. We show that the proposed method is effective for the fabrication of bent plates with low cost.

• Proceeding of EDISON Challenge
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• 2012.04a
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• pp.77-80
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• 2012

초음속 흡입구는 설계점에서 안정적으로 작동하지만 설계점 밖에서는 엔진성능이 급격히 감소하거나 층 격파 불안정 문제가 발생할 수 있다. 초음속 흡입구의 일반적인 특성을 파악하기 위해 2단 꺾임각을 갖는 외부 압축식 2차원 흡입구를 설계하고 EDISON_열유체 시스템을 이용하여 최종적으로 설계 마하수 2.5에서 작동하는 형상을 얻었다. 그러나 설계 마하수 이하의 영역에서는 충격파-경계층, 충격파간 상호작용으로 인해 유동에서 박리가 발생하고 최종적으로 흡입구 목을 질식시켜 아임계 상태로 천이된다. 이를 해결하기 위해 유동 제어 방법 중 하나인 bleeding을 이용하여 경계층을 제거하거나 유동의 박리를 방지하여 충격파를 cowl lip 전방에 안정하게 고정시킬 수 있었으며, 결과적으로 목적하였던 마하수 2.0에서 2.5에 이르는 작동 영역에서 강건하게 운용될 수 있는 초음속 흡입구를 설계하였다.

• Proceedings of the Korean Operations and Management Science Society Conference
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• 1995.04a
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• pp.617-628
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• 1995

본 논문에서는 상용화된 이 기종 CAD/CAM 시스템간의 CAD 데이타 교환기능을 가지는 IGES Translator 시스템의 구조를 제안한다. 제품생산의 여러 단계에서 CAD/CAM의 사용이 보편화되어감에 따라 상용 CAD/CAM 시스템들은 응용분야에 맞는 특수한 도구로 사용되는 경향이 생겨났다. 예를 들어, ALIAS는 주로 스타일링 디자인에, I-DEAS와 PRO/ENGINEER는 엔지니어링 디자인에, EUCLID는 금형 디자인에, 그리고 OMEGA와 Z-MASTER는 NC 공구경로생성에 주로 사용되고 있다. CAD 데이타 교환을 위해 제안된 중립파일형식(Neutral File Format)중에서, IGES(Initial Graphics Exchange Specification)는 대부분의 상용 CAD/CAM 시스템에서 지원을 하고 있으며 가장 널리 쓰이는 파일형식이다. 그런데, IGES를 통한 CAD 데이타 교환은 다음과 같은 문제점들을 가지고 있다. 즉, patch의 사라짐, 경계곡선의 왜곡, patch의 overlap 또는 gap, trimming error, 곡면각의 꺾임각도 등이 그것이다. 이 논문의 목적은 이러한 문제점들을 해결할 수 있는 범용 IGES Translator를 개발하는데 있다. 이 논문의 주요한 기여 내용은 다음과 같다. 1) 주요 상용 CAD/CAM 시스템의 IGES Interface 기능의 비교 분석, 2) 주요 상용 IGES Translator의 기능 분석, 3) 사용자의 기능적 요구사항의 분석, 4) 사용자 관점 및 시스템 관점에서의 IGES Translator의 구조 제안, 5) Prototype IGES Translator의 개발 및 테스트 결과 제시.

• Fashion & Textile Research Journal
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• v.14 no.6
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• pp.952-959
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• 2012

This study looks into the changes in collar patterns in tailored jackets with different numbers of buttons. The study discusses the pattern design method of tailored colors in 4 different styles, such as the effect of the number of buttons of tailored jackets on collar width and length, lapel width and length, and angle of lapel and overall balance in design. Through the first dress experiment, patterns were adjusted and corrected. The second dress experiment was conducted with the modified experimental clothes. The results of comparison and analysis are as follows. The 1 button tailored jacket was most preferred for its beautiful expression and overall balance of upper color and lapel when its lapel width was 7.5 cm. The second most preferred one was the 2 button tailored jacket with lapel width of 8 cm, and the 3 button jacket showed relatively good balance when its lapel width was 7.5 cm. The 4 button tailored jacket showed a bad balance in collar and button. Also, its overall silhouette was disappointing and thus was less preferred than others. For smaller number of buttons, the angle of lapel's break line increased, thus displaying a more refined and slim silhouette. On the other hand, the angle of lapel's break line decreased for greater number of buttons, thus displaying a dull and fat image. As a result, the jacket with many buttons was less preferred.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.5
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• pp.12-18
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• 2006

A new steady approach has been developed to predict the transonic buffet onset of a high speed aircraft. In this paper, the flow is assumed to be steady for the buffet onset. The present study involves the analysis of a distinct change in the variation of various static aerodynamic parameters. These distinct changes indicates the onset of transonic buffet. Among the various aerodynamic parameters considered in this study, the variation in the center of pressure has shown to provide a clearest indicator of transonic buffet onset. This new steady approach can be applied to predict the transonic buffet onset for airfoils with shock induced separation bubble and for large swept wings with small aspect ratios. Good agreements have been obtained compared with unsteady wind tunnel buffet test data. Based on the results obtained the new steady approach, it can be newly suggested that the distinct slope changes of the center of pressure curve can be used as an indicator of buffet onset for the steady experimental method on a full aircraft configuration.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.16 no.8
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• pp.5051-5059
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• 2015

Structural behaviour of the front loader for an agricultural tractor was analyzed for three impact test conditions: drop and catch, corner pull, and corner push. Rigid-body dynamic, transient structural, and static structural analyses were conducted using a commercial finite element software. Analysis of the drop and catch test dealt with the case that the bucket located at the maximum elevation was dropped and catched through three steps. Analysis of the corner pull test dealt with the case that the bucket constrained to the ground by a chain at its corner was raised suddenly. Analysis of the corner push test dealt with the case that the corner of the bucket collided with an obstacle. Results of analyses of the three test conditions showed that maximum stress occurs at the geometrically discontinuous location in the mount and is caused from local stress concentration. Results of the present research can be utilized as a guideline to achieve more reliable and safe structural design of the front loaders.