• Title/Summary/Keyword: take-off

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The Determination of Take-Off Time in Iteration on Dynamic Susceptibility Contrast Agent MR Perfusion Imaging

  • 김대원;류완석;정성택
    • Proceedings of the KSMRM Conference
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    • 2003.10a
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    • pp.79-80
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    • 2003
  • In existing method, the threshold has determined the points to be used in extrapolation and only pre-peak points were used to find t0. However, to reduce error in using this fitting method, in this study, finding t0is considered the correlation between fitting result and each profile in using iteration method. And the proposed method is compared with the existing method.

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Relationship between Take-off Behavior of Hard-disk Slider and AE Signal (하드디스크 슬라이더의 부상 특성과 AE신호의 관계)

  • 이상민;문재택;김대은
    • Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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    • 1999.11a
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    • pp.310-317
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    • 1999
  • Acoustic emission(AE) signal has been widely utilized to monitor the interaction at the head/disk interface. In this work the relationship between the AE signal and the state of contact between the slider and the disk is presented. Results of the FFT analyses of the AE signal could be used to better understand the interfacial interaction. Also, it was found that wear particles affect the AE signal. Therefore, the signal can be used to monitor the wear particle presence at the interface.

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A study of the noise suppression system at the aircraft ground run-up test room (항공기 지상실험에 의한 소음 저감 방안에 관한 연구)

  • 김인수;고철수;김형근
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2003.11a
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    • pp.718-723
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    • 2003
  • The number of jet aircraft is increasing. The aircraft noise making people near airports nervous have become a serious social problem. The aircraft noise can be classified into two groups; noise being generated at take-off or landing and noise form run-up test on the ground. In this paper, we consider the aircraft noise from run-up test on the pound and we suggest the noise suppression system.

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FPD Industry, Challenge for Value Creation

  • Chang, Won-Kie
    • 한국정보디스플레이학회:학술대회논문집
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    • 2009.10a
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    • pp.1-1
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    • 2009
  • Recently, the FPD industry has faced the limit in market growth due to lack of new growth engine as a replacement of television. With sluggish market demand deepened by global economic crisis and persistent concern over panel oversupply, growth of the panel market has sharply slowed down, and profitability has been eroded. This also has tremendous effect on related industries including component, material and machine industries, spreading a sense of crisis across the whole FPD industry. Under this circumstance, for the FPD industry to take off once again, all involved in the FPD industry must cooperate and come up with innovative ideas, and identify the driving force to realize turbo-charged growth.

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Preprocessing for Tracking of Moving Object (이동 물체 추적을 위한 전 처리)

  • 홍승범;백중환
    • Proceedings of the Korea Institute of Convergence Signal Processing
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    • 2003.06a
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    • pp.82-85
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    • 2003
  • This paper proposes a preprocessing method for tracking aircraft's take-off and lading. The method uses accumulative difference image technique for segmenting the object from the background, and obtains the centroid of the object exactly using centroid method. Then the moving object is analyzed and represented with the information such as feature point, velocity, and distance. A simulation result reveals that the proposed algorithm has good performance in segmenting and tracking the aircraft.

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The Study on the Minimum Requirements for the Design of an Airpark used in Light Sport Aircraft Operations (경량항공기 이착륙장의 최소 요구조건에 대한 연구)

  • Shin, Dai-Won;Shin, Hong-Chul
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.17 no.2
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    • pp.18-22
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    • 2009
  • In this study, we surveyed the operating status of the Light Sport Aircraft(LSA) in Korea, and reviewed the minimum requirements of the airpark for LSA in other countries. Based on the information, we presented the airpark standards to ensure the safe take-off, landing, and operation of LSA in Korea.

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Career Development Experience of Youth in Late Adolescence who Entered a Different University after Taking a Semester off (반수로 대학에 진학한 후기 청소년들의 진로발달 경험 : 도돌이표를 지나도 반복되는 길)

  • Kim, Seo Hyun;Yim, Hye Rim;Myung, So Yeon;Chung, Ick-Joong
    • Korean Journal of Social Welfare Studies
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    • v.47 no.4
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    • pp.183-216
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    • 2016
  • This study aims to investigate the career development experience of youth in late adolescence who entered a different university after taking a semester off (as known as Bansu in Korean), in depth, applying a phenomenological research method. For the research, this study selected seven adolescents as research participants to reveal the essential meaning of their experience, vividly. The data were analyzed by Giorgi's method to draw components of the experience of research participants. As a result of the research, the career development experience of youth in late adolescence who entered a different university after taking a semester off was systematized into 19 sub-categories and structured into four main categories: "high school years in which academic record was more important than aptitude", "the step away from the dream, being forced to proceed to college", "the time of study to take the exam again, which was an advantage and disadvantage at the same time" and "the wish unfulfilled even with the success of entering a different university." It turned out that the main topic was "the repeated way even after passing the repeat sign." They took the College Scholastic Ability Test (CSAT) once again and came back to the narrow way to enter a prestigious university, but they still compromised the standard made by the older generation. This study has significance for late adolescents' welfare and happiness in that it explored the in-depth meanings of the career development experience of youth who entered a different university by taking the CSAT again after taking a semester off. Lastly, based upon the situation of the increase in the number of students who take the CSAT again, this study suggested better measures for career development during adolescence and the promotion of their quality of life.

A Proof of Concept Investigation on a Pendular Power Take-Off System of Horizontal Wave Power Generator (수평파력 발전장치의 진자형 1차 에너지 추출 시스템에 대한 기초 모형실험 및 시뮬레이션)

  • Park, Yong-Kun;Lim, Chae Gyoung
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.18 no.9
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    • pp.68-75
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    • 2017
  • This paper presents the experimental and theoretical results of the dynamic responses of a pendular energy extractor in a two-dimensional wave channel. By adopting a wave maker with varying wave height and period, the dynamic responses of the pendular buoy were experimentally obtained. Furthermore, with the aid of the co-simulation of moving particle analysis and rigid dynamic analysis, the dynamic responses of the pendular system were evaluated. In order to validate the feasibility of the proposed wave power generator, the force tuning of the pendular system with restoring energy was carried out. The results provide proof of concept data for the development and design of a commercial model for horizontal wave power generators in the shoreline area.

Flow Characteristics of WIG-Effect Vehicle with Direct-Underside-Pressurization System and Propeller (DUP와 프로펠러가 있는 위그선 주위의 유동특성)

  • Lee, Ju-Hee;Kim, Byeong-Sam;Park, Kyoung-Woo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.34 no.6
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    • pp.649-654
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    • 2010
  • A three-dimensional numerical study of the WIG-effect vehicle with a direct-underside-pressurization (DUP) system and a propeller is performed to analyze the aerodynamic forces and moments acting on the vehicle. The computational model includes all the compartments of a WIG-effect vehicle, including a propeller in the middle of the fuselage and an air chamber under the fuselage. The DUP system and propeller help considerably reduce the take-off speed and minimize the effect of the hump drag when the vehicle accelerates to take off on water. The airflow is accelerated by a propeller, and the air then enters the air chamber through a channel in the middle of the fuselage, this air helps increase the lift since the dynamic pressure of air is converted to static pressure. However, the air accelerated by the propeller produces excessive drag and creates yawing moment. It is found that the effect of yawing and rolling moments on static stability is negligible.