• Title/Summary/Keyword: 측면방향

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A study on micropipes and the growth morphology in 6H- SiC bulk crystal (6H - SiC bulk 단결정 성장 양상과 micropipe에 관한 연구)

  • 강승민;오근호
    • Journal of the Korean Crystal Growth and Crystal Technology
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    • v.5 no.1
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    • pp.44-49
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    • 1995
  • Abstract The surface of 6H - SiC bulk crystal grown by sublimation process was investigated by optical microscope observation. Since, in the 6H crystal growing, the crystal had the habitual step growth attitude such that the lateral growth rate along the random a - axis orientation was higher than that along the c - axis of the growth direction, then many steps were developed. There were, also, many micropipes on the surface in the form of as-like large voids. However, they were differenciated with pores and cross- sectional shape of them were close to the circle. In this study, many micropipes, planar defects and the growth steps appeared on the grown crystal surface were investigated.

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A Study on Crashworthiness Optimization of Front Side Members using Bead Shape Optimization (비드 형상 최적화를 이용한 전방 측면 부재의 충돌 최적화 연구)

  • Lee, Jun-Young;Lee, Jung-Suk;Lee, Yong-Hoon;Bae, Bok-Soo;Kim, Kyu-Hak;Yim, Hong-Jae
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.36 no.3
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    • pp.331-337
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    • 2012
  • In this study, the front side member is optimized using a topography optimization technique. Optimization of a simple beam is conducted before optimization of the front side member. The objective function is set to minimize the first buckling factor in the longitudinal direction. The design variable corresponds to the perturbation of nodes normal to the shell's mid-plane space. The crash analysis is conducted on a simple beam, which is optimized by Response Surface Method and the topography optimization technique. In order to verify the topography optimization technique, the results of the RSM and topography optimization model are compared. Consequently, we confirm the satisfactory performance of the topography optimization technique, and apply this topography optimization to the front side member. Thus, the front side member is optimized and its crashworthiness is increased.

A Development of Evaluation Criteria for the Expressway Service Areas From Users Point of View (고속도로 휴게시설 이용자측면의 서비스 평가지표 개발)

  • Kim, Hyung-Kyu;Chio, Hyoung-Sun;Park, Wan-Yong;Won, Jai-Mu
    • International Journal of Highway Engineering
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    • v.14 no.3
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    • pp.121-130
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    • 2012
  • This study develops the evaluation model which is for assessing on the side of users in expressway service areas. The direction of development on Evaluation Criteria is all about on the side of necessity of service area users, the reflection of current conditions, the construction of total evaluation criteria, and the examination of connecting study with current study. After that, this study examines previous evaluation criterias and researchers will select the primary provision of evaluation through FGI, and they derive the final evaluation criteria throughout the verification of suitability on Evaluation Criteria. Throughout AHP analysis which is a professional survey system of users, researchers derive on the side of facilities, on the side of operations, on the side of environments, and on the side of services in order by the weightings.

Analysis of the Interaction Between Hypersonic Free Stream and Side Jet Flow Using a DSMC Method (직접모사법을 이용한 극음속 대기 유동과 측면 제트의 상호 작용 해석)

  • Kim, Min-Gyu;Kwon, Oh-Joon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.3
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    • pp.1-9
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    • 2005
  • The interaction between hypersonic free stream and side jet flow at high altitudes is investigated by using the direct simulation Monte Carlo (DSMC) method. In order to alleviate the difficulty associated with the large density difference between the free stream and the side jet flow and to simulate the two flows simultaneously, a weighting factor technique is applied. For validation, the corner flow over a pair of plates perpendicularly attached is calculated with and without a side jet, and the results are compared with experiment. For a more realistic configuration, the flow past a blunted cone cylinder shape is solved. The leeward or windward jet is injected into the free stream and the effect on the aerodynamic force and moment is observed at various flow angles. The lambda shock effect and the wake structure are studied in terms of the surface pressure differential. A higher interaction between the free stream and the side jet flow is observed when the side jet is injected in the windward direction.