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    다양한 마하수 영역의 유동 해석을 위한 Coupled 방식의 개선된 속도-압력-엔탈피 연계 알고리즘

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    https://www.riss.kr/link?id=A106095046

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    다국어 초록 (Multilingual Abstract) kakao i 다국어 번역

    In this paper, a pressure-based coupled computational fluid dynamics algorithm for numerical analysis of all mach number region flow is developed. For this purpose, an enhanced pressure based coupled algorithm was developed through the pressure-velocity coupled algorithm and the pressure-enthalpy coupled algorithm were combined. In additional, the Kurganov-Tadmor flux splitting scheme, which is mainly used in density-based solvers, was applied to a developed pressure-based coupled solver. To confirm the analytical ability of developed solver, the variety of mach number flow problems were performed using the developed solver. It was confirmed that the developed solver had the similar analytical ability with that of the other numerical codes through the analysis of the shock tube problems. In order to verify the analytical ability for the variety mach number flow region of the developed solver, 2D bump and nozzle problems and 3D missile problem were analyzed and compared with results of experiments and other numerical analysis codes. It is confirmed that the analytical ability of developed solver in the all speed flow region is somewhat improved than the commercial analysis package and is similar to the density based in-house CFD code.
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    In this paper, a pressure-based coupled computational fluid dynamics algorithm for numerical analysis of all mach number region flow is developed. For this purpose, an enhanced pressure based coupled algorithm was developed through the pressure-veloci...

    In this paper, a pressure-based coupled computational fluid dynamics algorithm for numerical analysis of all mach number region flow is developed. For this purpose, an enhanced pressure based coupled algorithm was developed through the pressure-velocity coupled algorithm and the pressure-enthalpy coupled algorithm were combined. In additional, the Kurganov-Tadmor flux splitting scheme, which is mainly used in density-based solvers, was applied to a developed pressure-based coupled solver. To confirm the analytical ability of developed solver, the variety of mach number flow problems were performed using the developed solver. It was confirmed that the developed solver had the similar analytical ability with that of the other numerical codes through the analysis of the shock tube problems. In order to verify the analytical ability for the variety mach number flow region of the developed solver, 2D bump and nozzle problems and 3D missile problem were analyzed and compared with results of experiments and other numerical analysis codes. It is confirmed that the analytical ability of developed solver in the all speed flow region is somewhat improved than the commercial analysis package and is similar to the density based in-house CFD code.

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    참고문헌 (Reference)

    1 한상훈, "압축성 코드에서 예조건화 코드로의 이전" 한국항공우주학회 35 (35): 183-195, 2007

    2 김태우, "압축성 유동 해석을 위한 압력 기반 해석자의 개선된 알고리즘 개발" 한국전산유체공학회 22 (22): 28-35, 2017

    3 Lax, P.D., "Weak solutions of nonlinear hyperbolic equations and their numerical computation" 7 : 159-193, 1954

    4 Cuffel, R.F., "Transonic Flowfield in a Supersonic Nozzle with Small Throat Radius of Curvature" 7 (7): 1364-1366, 1969

    5 Choi, Y., "The appilcation of Preconditioning in Viscous Flows" 107 : 207-223, 1993

    6 Graves, E.B., "Stability And Control Characteristics At Mach Numbers From 0.20 To 4.63 Of A Cruciform Air-To-Air Missile With Triangular Canard Controls And A Trapezoidal Wing" NASA Technical Memorandum 1974

    7 Emans, M., "SIMPLE-H: a finite-volume pressure-enthalpy coupling scheme for flows with variable density" 69 (69): 206-, 2012

    8 Patankar, J., "Numerical heat transfer and fluid flow" CRC press 1980

    9 Shu, C.-W., "Numerical experiments on the accuracy of ENO and modified ENO schemes" 5 (5): 127-149, 1990

    10 Kim, S.D., "Comparison of Low-Mach number fixing methods for Roe scheme" 2012

    1 한상훈, "압축성 코드에서 예조건화 코드로의 이전" 한국항공우주학회 35 (35): 183-195, 2007

    2 김태우, "압축성 유동 해석을 위한 압력 기반 해석자의 개선된 알고리즘 개발" 한국전산유체공학회 22 (22): 28-35, 2017

    3 Lax, P.D., "Weak solutions of nonlinear hyperbolic equations and their numerical computation" 7 : 159-193, 1954

    4 Cuffel, R.F., "Transonic Flowfield in a Supersonic Nozzle with Small Throat Radius of Curvature" 7 (7): 1364-1366, 1969

    5 Choi, Y., "The appilcation of Preconditioning in Viscous Flows" 107 : 207-223, 1993

    6 Graves, E.B., "Stability And Control Characteristics At Mach Numbers From 0.20 To 4.63 Of A Cruciform Air-To-Air Missile With Triangular Canard Controls And A Trapezoidal Wing" NASA Technical Memorandum 1974

    7 Emans, M., "SIMPLE-H: a finite-volume pressure-enthalpy coupling scheme for flows with variable density" 69 (69): 206-, 2012

    8 Patankar, J., "Numerical heat transfer and fluid flow" CRC press 1980

    9 Shu, C.-W., "Numerical experiments on the accuracy of ENO and modified ENO schemes" 5 (5): 127-149, 1990

    10 Kim, S.D., "Comparison of Low-Mach number fixing methods for Roe scheme" 2012

    11 Mangani, L., "An OpenFOAM pressure-based coupled CFD solver for turbulent and compressible flows in turbomachinery applications" 69 (69): 413-, 2016

    12 Wee, H.C., "Aerodynamic Analysis Of A Canard Missile Configuration Using Ansys-Cfx" Naval Postgraduate School 2011

    13 Kraposhin, M., "Adaptation of Kurganov-Tadmor Numerical Scheme For Applying in Combination With the PISO Method in Numerical Simulation of Flows in a Wide Range of Mach Numbers" 66 : 43-52, 2015

    14 Sod, G.A., "A survey of several finite difference methods for systems of non-linear hyperbolic conservation laws" 27 (27): 1-159, 1978

    15 Emans, M., "A novel SIMPLE-based pressure-enthalpy coupling scheme for engine flow problems" 17 (17): 1-, 2012

    16 Rieper, F., "A low-Mach number fix for Roe’s approximate Riemann solver" 230 : 5263-5287, 2011

    17 Darwish, M., "A Fully Coupled Navier-Stokes Solver for Fluid Flow at All Speeds" 65 (65): 410-, 2014

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    2027 평가 재인증평가 신청대상 (재인증)
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    2005-06-16 학술지명변경 외국어명 : Jpurnal of Computatuonal Fluids Engineering -> Korean Society of Computatuonal Fluids Engineering KCI등재후보
    2005-01-01 등재 등재후보 1차 PASS (등재후보1차) KCI등재후보
    2004-01-01 등재 등재후보 1차 FAIL (등재후보1차) KCI등재후보
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