• 제목/요약/키워드: Modified Garabedian-McFadden method

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Modified Garabedian-McFadden 방법을 이용한 프로펠러 날개 단면의 역설계 기법 (The Inverse Design Technique of Propeller Blade Sections Using the Modified Garabedian-McFadden Method)

  • 정철민;조장근;박원규
    • 대한조선학회논문집
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    • 제36권4호
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    • pp.28-36
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    • 1999
  • 본 연구에서는 MGM(Modified Grrabedian-McFadden)방법에 기초한 효율적인 역설계 방법을 개발하였다. 표면압력 분포를 얻기 위해 2-D Navier-Stokes 방정식을 풀었고, 역설계를 수행하기 위해 MGM방법을 사용하였다. MGM 방법은 설계 목적 압력분포와 Navier-Stokes 방정식에서 계산된 압력분포의 차인 잔여량을 보정하는 잔여-보정 기법이다. 코드 개발을 위하여 몇몇 익형과 프로펠러 형상설계에 적용하였다. 이들 모두 목표하는 형상에 잘 수렴해 갔다.

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병렬 연산을 이용한 축류 블레이드의 역설계 (The Inverse Design Technique of Axial Blade Using the Parallel Calculation)

  • 조장근;안재성;박원규
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 1999년도 유체기계 연구개발 발표회 논문집
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    • pp.200-207
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    • 1999
  • An efficient inverse design technique based on the MGM (Modified Garabedian-McFadden) method has been developed. The 2-D Navier-Stokes equations are solved for obtaining the surface pressure distributions and coupled with the MGM method to perform the inverse design. The solver is parallelized by using the domain decomposition method and the standard MPI library for communications between the processors. The MGM method is a residual-correction technique, in which the residuals are the difference between the desired and the computed pressure distribution. The developed code was applied to several airfoil shapes and the axial blade. It has been found that they are well converged to their target pressure distribution.

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원통형 수중운동체 두부 형상 역설계 (An Inverse Design for Nose Shape of a Cylindrical-Shaped Submerged Body)

  • 정철민
    • 한국군사과학기술학회지
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    • 제7권3호
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    • pp.69-76
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    • 2004
  • In this paper, an efficient inverse design method for nose shape of submerged body based on the MGM(Modified Garabedian-McFadden) design method has been developed. The MGM design method is a residual-correction technique, in which the residuals are differences between the desired and the computed pressure distributions. 3-D incompressible Wavier-Stokes equation was adopted for obtaining the surface pressure distribution and combined with the MGM design method to perform the inverse design of nose shape of submerged body. The design method was verified by applying to several airfoil shapes. Improved design shapes could be obtained when the method was applied to nose shapes of submerged body.