• Title/Summary/Keyword: 전산유체공학

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CFD Applications on Aerodynamic Design and Analysis of Missiles (유도무기 형상설계/공력해석에 대한 CFD 응용)

  • Ahn C. S.;Hong S. K.
    • 한국전산유체공학회:학술대회논문집
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    • 2003.08a
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    • pp.114-119
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    • 2003
  • 지난 20여년간 전산유체역학은 알고리즘의 개발뿐만 아니라 컴퓨터의 성능 향상에 힘입어 많은 발전을 거듭하여 이제는 유체역학의 한 분야로서 필수적인 학문이 되었다. ADD의 유도무기 개발에 있어 형상설계 및 공력해석의 업무는 사업도출 직후 초반시점부터 수행하여 할 아주 중요한 연구 분야이다. 또한 구조, 제어공학 및 구동분야와 연계된 공력자료를 생산하여 제공하는 데 있어 CFD를 응용하여 많은 공학적인 난제를 해결하고 있다. 이에 관련된 기술적인 CFD의 역할 및 기여도에 대하여 소개하고자 한다.

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Study of Vortex Generator for Aerodynamic Improvement (공력특성 향상을 위한 와류발생기에 대한 고찰)

  • Kim, Cheol-Wan;Shim, Jae-Yeol;Kim, Eung-Tai;Lee, Dae-Sung
    • 한국전산유체공학회:학술대회논문집
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    • 2008.03b
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    • pp.483-486
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    • 2008
  • Numerical Simulation was performed to investigate the role of vortex generator. Vortex generator installed on the upper surface of the wing, generates vortex flow, mimic the external flow with boundary layer flow and transfer energy from outside to wall boundary. Vortex generator, thus, retards the flow separation and increases the lift and drag of the wing.

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Computational Fluid Dynamics for Proton Exchange Membrane Fuel Cell (PEMFC) (고체고분자전해질연료전지의 해석을 위한 전산유체역학)

  • Kim, Sunhoe
    • Prospectives of Industrial Chemistry
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    • v.22 no.4
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    • pp.20-34
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    • 2019
  • 수소경제 시대의 도래와 함께 연료전지에 관한 연구가 크게 주목받고 있다. 그중 실험적으로 분석이 어려운 부분에 관하여 비용과 시간이 요구되는 실험적인 방법을 배제할 수 있는 모델링 기법인 전산유체역학(computational flow dynamics, CFD)이 큰 관심을 받고 있다. 연료전지의 연구에 주로 사용되는 전산유체역학에 관한 연구는 열분포, 유체의 흐름, 각종 반응물의 농도, 그리고 전기화학반응 등의 실험적인 분석이 현실적으로 불가능한 부분의 분석으로 통하여 실험을 줄이고도 많은 결과를 얻을 수 있는 연구가 활발하게 진행되고 있다. 본 기고문에서는 전산유체역학을 이용한 연료전지 내부에서 벌어지고 있는 각종 유체, 열, 전기화학반응 등에 관한 연구동향을 소개하고자 한다.

Application of MSAP to JDAM Separation from an F/A-18C Aircraft (MSAP을 이용한 F/A-18C로 부터 JDAM 분리 해석)

  • Lee Seungsoo
    • Journal of computational fluids engineering
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    • v.9 no.1
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    • pp.41-47
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    • 2004
  • A successful store separation analysis tool, MSAP(Multi-body Separation Analysis Program) has been applied to F/A-18C/JDAM CFD Challenge Ⅱ. The challenge was devised to challenge CFD community to use CFD methodologies to predict and match the trajectory of a JDAM MK-84 separating from F/A-l8C. Trajectory simulations for two flight conditions were performed. Comparison between computed and measured flight trajectories for both conditions shows a good agreement.

DEVELOPMENT OF THE PRE-PROCESSOR FOR CFD (CFD용 전처리장치 개발)

  • Kim, S.R.
    • Journal of computational fluids engineering
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    • v.18 no.2
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    • pp.72-77
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    • 2013
  • The Pre-processor program for CFD is being developed using wxWidgets and OpenGL libraries. This program can be run on both Windows and Linux operating systems. Undergraduate students and beginners can learn and use this very easily by menu and templates. Until now, structured mesh can be created in Cartesian or Cylindrical coordinates. This program will be used easily to make various type of meshes using templates.

Code Development for Two-Dimensional Flow Visualization (객체지향형 2차원 유동 가시화 코드 개발)

  • Sah Jong-Youb;Huh Jun-Sung
    • Journal of computational fluids engineering
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    • v.8 no.1
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    • pp.30-37
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    • 2003
  • The post-processor for two-dimensional flow visualization has been developed by using OOP(object-oriented programming) of Visual C++. User-friendly GUI(graphic user interface) has been built on the base of MFC(Microsoft Foundation Class). The number and order of variables can be specified by user because the input style is the free-format. The new variable can be defined and added to the variable list by using the various operators and functions.

CHARACTERISTIC OF BUTTERFLY VALVE FLOW WITH DIFFERENT DESIGN FACTORS (설계인자 변경에 따른 버터플라이 밸브 유동 특성에 관한 연구)

  • Lee, J.W.;Choi, H.K.;Yoo, G.J.
    • Journal of computational fluids engineering
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    • v.15 no.1
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    • pp.64-70
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    • 2010
  • Flow control butterfly valve(FCBV) is known to have difficulty in controlling flow rate along valve opening due to its high flow rate. In low opening condition, the butterfly valve also has some shortcomings such as noise, vibration and erosion which are mostly caused by cavitation effects. Therefore, the FCBV requires proper remedies to reduce cavitation effects and to improve flow control performance. Numerical analysis is applied to FCBV flow to find effects of design factors such as seat diameter and valve opening rate. Cases with 3 different sizes of seat diameter and various valve opening rate are selected for the numerical analysis. From the analysis results, it is found that the FCBV with small seat diameter shows better pressure loss performance and reduced cavitation effects.

NUMERICAL STUDY ON THE MIXER TYPES OF UREA-SCR SYSTEM FOR FLOW MIXING IMPROVEMENT (Urea-SCR 시스템에서 유동혼합 개선을 위한 혼합기 형상에 관한 수치적 연구)

  • Lee, J.W.;Choi, H.K.;Yoo, G.J.
    • Journal of computational fluids engineering
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    • v.15 no.4
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    • pp.9-16
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    • 2010
  • To alleviate NOx emission, a variety of approaches has been applied. In marine diesels, the application of SCR systems has been considered an effective exhaust aftertreatment method for NOx emission control. Most current SCR systems use a various catalyst for the reaction of ammonia with NOx to form nitrogen and water. In theory, it is possible to achieve 100% NOx if the $NH_3$-to-NOx ratio is 1:1. However, the reaction has a limited non-uniformity of the exhaust gas flow and ammonia concentration distribution. Therefore, it is necessary to investigate the optimum flow conditions. In order to achieve uniform flow at monolith front face, we are equipped with a various mixed devices. In this paper, it is presented that the mixed devices play an important role improvement of flow patterns and particle distributions of $NH_3$ by numerical simulation.