• 제목/요약/키워드: Re-Engineering

검색결과 3,536건 처리시간 0.026초

A Real-Time Virtual Re-Convergence Hardware Platform

  • Kim, Jae-Gon;Kim, Jong-Hak;Ham, Hun-Ho;Kim, Jueng-Hun;Park, Chan-Oh;Park, Soon-Suk;Cho, Jun-Dong
    • JSTS:Journal of Semiconductor Technology and Science
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    • 제12권2호
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    • pp.127-138
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    • 2012
  • In this paper, we propose a real-time virtual re-convergence hardware platform especially to reduce the visual fatigue caused by stereoscopy. Our unique idea to reduce visual fatigue is to utilize the virtual re-convergence based on the optimized disparity-map that contains more depth information in the negative disparity area than in the positive area. Our virtual re-convergence hardware platform, which consists of image rectification, disparity estimation, depth post-processing, and virtual view control, is realized in real time with 60 fps on a single Xilinx Virtex-5 FPGA chip.

A numerical investigation of the effects of Reynolds number on vortex-induced vibration of the cylinders with different mass ratios and frequency ratios

  • Kang, Zhuang;Zhang, Cheng;Chang, Rui;Ma, Gang
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제11권2호
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    • pp.835-850
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    • 2019
  • The numerical simulations for the Vortex-induced Vibration (VIV) of the cylinders with different combinations of mass ratio and frequency ratio were performed under the Reynolds (Re) number ranges of 1450-10200, 5800-40800 and 13050-91800 by using the embedded programs in OpenFoam. By combining with the modified SST k-ω turbulence model, the coupled Unsteady Reynolds-Average Navier-Stokes equations and double-degree-of-freedom vibration equations were solved. After analyzing the results, it is found that the some characteristics of the VIV have changed with the increase of the range of Re number, and the effects of Re number on vibration characteristics are also different under different combinations of mass ratio and frequency ratio. On this basis, the influence law of Re number on the characteristics of VIV of the cylinders is summarized, which can provide a reference for the research of VIV under higher Re number.

레거시 시스템의 재사용을 위한 RUP 기반의 효율적 재공학 프로세스 (An Efficient Reengineering Process based on RUP for Reusing Legacy Systems)

  • 최일우;류성열
    • 한국정보과학회논문지:소프트웨어및응용
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    • 제29권9호
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    • pp.619-630
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    • 2002
  • 1980년대 이후, 소프트웨어 위기에 대응하기 위한 다양한 소프트웨어 공학적 기법들이 출현하기 시작 하였고, 현재 소프트웨어의 질적 향상 및 생산성 향상을 꾀하기 위한 개발 지침으로 소프트웨어 컴포넌트 개발 프로세스를 구축하는데 관심이 집중되어지고 있다. 그러나 대부분의 방법론들이 앞으로 구축할 새로운 시스템의 재사용성 확보에 치중할 뿐, 실질적으로 기존 레거시 시스템의 자원을 재사용하여 새로운 시스템을 구축하는 방법은 효율적으로 지원하지 못하고 있는 실정이다. 본 논문에서는 레거시 시스템의 효율적 재사용을 위한 재공학 프로세스(Reengineering Process)로 RUP를 확장, 커스터마이징하여 구성한 RUP+re을 제시한다. RUP+re은 크게 역공학 워크플로우(Reverse Engineering Workflow), 재공학 워크플로우(Re-Engineering Workflow), 순공학 프로세스(Forward Engineering Process)로 구성되어진다. RUP+re의 각 워크플로우와 세부스텝을 제공하고 실사례 연구를 통하여 실질적으로 프로세스를 검증함으로서 레거시 시스템 자원의 재사용을 위한 소프트웨어 재공학 프로세스 구축에 효율적인 지침을 제공한다.

A simple method for estimating transition locations on blade surface of model propellers to be used for calculating viscous force

  • Yao, Huilan;Zhang, Huaixin
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제10권4호
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    • pp.477-490
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    • 2018
  • Effects of inflow Reynolds number (Re), turbulence intensity (I) and pressure gradient on the transition flow over a blade section were studied using the ${\gamma}-Re{\theta}$ transition model (STAR-CCM+). Results show that the $Re_T$ (transition Re) at the transition location ($P_T$) varies strongly with Re, I and the magnitude of pressure gradient. The $Re_T$ increases significantly with the increase of the magnitude of favorable pressure gradient. It demonstrates that the $Re_T$ on different blade sections of a rotating propeller are different. More importantly, when there is strong adverse pressure gradient, the $P_T$ is always close to the minimum pressure point. Based on these conclusions, the $P_T$ on model propeller blade surface can be estimated. Numerical investigations of pressure distribution and transition flow on a propeller blade section prove these findings. Last, a simple method was proposed to estimate the $P_T$ only based on the propeller geometry and the advance coefficient.

Thermoelectric Properties of Fe-doped $CoSb_3$ Prepared by Encapsulated Induction Melting and Hot Pressing

  • Park, Kwan-Ho;Kim, Mi-Jung;Jung, Jae-Yong;You, Sin-Wook;Lee, Jung-Il;Ur, Soon-Chul;Kim, Il-Ho
    • 한국분말야금학회:학술대회논문집
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    • 한국분말야금학회 2006년도 Extended Abstracts of 2006 POWDER METALLURGY World Congress Part 1
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    • pp.686-687
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    • 2006
  • The encapsulated induction melting and hot pressing were employed to prepare Fe-doped $CoSb_3$ skutterudites and their thermoelectric properties were investigated. Single phase $\delta-CoSb_3$ was successfully obtained by the subsequent heat treatment at 773K for 24 hours. Iron atoms acted as electron acceptors by substituting cobalt atoms. Thermoelectric properties were remarkably improved by the appropriate doping. $Co_{0.7}Fe_{0.3}Sb_3$ was found as an optimum composition for best thermoelectric properties in this work.

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ReMnO3(Re:Ho, Er) 박막의 강유전성에 미치는 열처리 공정의 영향 (Effects of Thermal Heat Treatment Process on the Ferroelectric Properties of ReMnO3 (Re:Ho, Er) Thin Films)

  • 김응수;채정훈
    • 한국세라믹학회지
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    • 제42권11호
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    • pp.763-769
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    • 2005
  • Ferroelectric $ReMnO_3$(Re:Ho, Er) thin films were deposited on Si(100) substrate by Metal-Organic Chemical Vapor Deposition (MOCVD). Crystallinity and electric properties of $ReMnO_3$(Re:Ho, Er) thin films were investigated as a function of thermal heat treatment process, CHP (Conventional Heat-treatment Process) and RTP (Rapid Thermal Process). $ReMnO_3$(Re:Ho, Er) thin films prepared by RTP showed higher c-axis preferred orientation and homogeneous surface roughness than those prepared by CHP. The remnant polarization of ferroelectric hysteresis loop of $ReMnO_3$(Re:Ho, Er) thin films was strongly dependent on the c­axis preferred orientation of hexagonal single phase, and the leakage current characteristics of thin films were dependent on the homogeneity of grain size as well as surface roughness of thin films.

재진입비행체의 궤적제어 (Trajectory Control for Re-entry Vehicle)

  • 박수홍;이대우
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1997년도 추계학술대회 논문집
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    • pp.361-364
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    • 1997
  • The re-enty guidance design involves trajectory optimization, generation of a reference drag acceleration profile with the satisfaction of trajectory constraints. This reference drag acceleration profile can be considered as the reference trajectory. This paper proposes the atmospheric re-entry system which is composed of longitudinal, later and range control. This paper shows the a performance of a re-entry guidance and control system using feedback linearization control and predictive control.

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