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      KCI등재

      하이퍼루프 차량 공력 해석을 위한 적합직교분해 기법 연구

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      https://www.riss.kr/link?id=A107778438

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      다국어 초록 (Multilingual Abstract) kakao i 다국어 번역

      The Proper Orthogonal Decomposition (POD) method was applied for enhancing the computational efficiency of aerodynamic simulations of hyperloop vehicle. At first, two dimensional axisymmetric computations of hyperloop vehicle were performed according to the vehicle speed and pressure inside tube in order to construct a snapshot dataset. Then, a reduced order model (ROM) was constructed through the POD method. For improvement of the accuracy of reconstructed dataset from ROM, POD basis weight coefficients were calculated by the artificial neural network. (ANN) By the comparison of original CFD data and reconstructed POD data, it was confirmed that the POD data follow the features of CFD data; the flow contours and pressure distributions of the POD data showed good agreement with CFD data. After ROM and POD basis weight coefficients by ANN are obtained, it can reconstruct the flow field data with new set of flow conditions quickly. Therefore, the POD method can be sufficiently used for the aerodynamic computations of hyperloop vehicle and ultimately design optimization problem of hyperloop system.
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      The Proper Orthogonal Decomposition (POD) method was applied for enhancing the computational efficiency of aerodynamic simulations of hyperloop vehicle. At first, two dimensional axisymmetric computations of hyperloop vehicle were performed according ...

      The Proper Orthogonal Decomposition (POD) method was applied for enhancing the computational efficiency of aerodynamic simulations of hyperloop vehicle. At first, two dimensional axisymmetric computations of hyperloop vehicle were performed according to the vehicle speed and pressure inside tube in order to construct a snapshot dataset. Then, a reduced order model (ROM) was constructed through the POD method. For improvement of the accuracy of reconstructed dataset from ROM, POD basis weight coefficients were calculated by the artificial neural network. (ANN) By the comparison of original CFD data and reconstructed POD data, it was confirmed that the POD data follow the features of CFD data; the flow contours and pressure distributions of the POD data showed good agreement with CFD data. After ROM and POD basis weight coefficients by ANN are obtained, it can reconstruct the flow field data with new set of flow conditions quickly. Therefore, the POD method can be sufficiently used for the aerodynamic computations of hyperloop vehicle and ultimately design optimization problem of hyperloop system.

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      참고문헌 (Reference)

      1 이희남, "적합직교분해를 이용한 2차원 실린더 후류 유동장 분석 및 재구성" 한국군사과학기술학회 13 (13): 164-169, 2010

      2 강형민, "적합직교분해 기법을 통한 하이퍼루프 차량의 공력 해석" 한국전산유체공학회 25 (25): 105-110, 2020

      3 강형민, "적합직교분해 기법에서의 효율적인 스냅샷 선정을 위한 고유값 분석" 한국전산유체공학회 22 (22): 59-66, 2017

      4 Park, K., "Reduced-order model with an artificial neural network for aerostructural design optimization" 50 (50): 1106-1116, 2013

      5 Walton, S., "Reduced order modelling for unsteady fluid flow using proper orthogonal decomposition and radial basis function" 37 : 8930-8945, 2013

      6 전상욱, "Reduced order model of three-dimensional Euler equations using proper orthogonal decomposition basis" 대한기계학회 24 (24): 601-608, 2010

      7 Zhang, L., "Multidisciplinary design optimization for a centrifugal compressor based on proper orthogonal decomposition and an adaptive sampling method" 8 (8): 1-21, 2018

      8 Musk, E, "Hyperloop Alpha"

      9 강형민, "A Study on the Aerodynamic Drag of Transonic Vehicle in Evacuated Tube Using Computational Fluid Dynamics" 한국항공우주학회 18 (18): 614-622, 2017

      1 이희남, "적합직교분해를 이용한 2차원 실린더 후류 유동장 분석 및 재구성" 한국군사과학기술학회 13 (13): 164-169, 2010

      2 강형민, "적합직교분해 기법을 통한 하이퍼루프 차량의 공력 해석" 한국전산유체공학회 25 (25): 105-110, 2020

      3 강형민, "적합직교분해 기법에서의 효율적인 스냅샷 선정을 위한 고유값 분석" 한국전산유체공학회 22 (22): 59-66, 2017

      4 Park, K., "Reduced-order model with an artificial neural network for aerostructural design optimization" 50 (50): 1106-1116, 2013

      5 Walton, S., "Reduced order modelling for unsteady fluid flow using proper orthogonal decomposition and radial basis function" 37 : 8930-8945, 2013

      6 전상욱, "Reduced order model of three-dimensional Euler equations using proper orthogonal decomposition basis" 대한기계학회 24 (24): 601-608, 2010

      7 Zhang, L., "Multidisciplinary design optimization for a centrifugal compressor based on proper orthogonal decomposition and an adaptive sampling method" 8 (8): 1-21, 2018

      8 Musk, E, "Hyperloop Alpha"

      9 강형민, "A Study on the Aerodynamic Drag of Transonic Vehicle in Evacuated Tube Using Computational Fluid Dynamics" 한국항공우주학회 18 (18): 614-622, 2017

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2027 평가예정 재인증평가 신청대상 (재인증)
      2021-01-01 평가 등재학술지 유지 (재인증) KCI등재
      2018-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2015-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2011-01-01 평가 등재 1차 FAIL (등재유지) KCI등재
      2009-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2006-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      2005-06-16 학술지명변경 외국어명 : Jpurnal of Computatuonal Fluids Engineering -> Korean Society of Computatuonal Fluids Engineering KCI등재후보
      2005-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
      2004-01-01 평가 등재후보 1차 FAIL (등재후보1차) KCI등재후보
      2002-07-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.2 0.2 0.19
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.16 0.15 0.405 0.05
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