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All-speed Two-phase Computations for General Equation of State with Preconditioning Techniques and Scaling of Numerical Dissipations

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dc.contributor.advisor김종암-
dc.contributor.author김현지-
dc.date.accessioned2017-07-14T03:37:35Z-
dc.date.available2017-07-14T03:37:35Z-
dc.date.issued2015-02-
dc.identifier.other000000026428-
dc.identifier.urihttps://hdl.handle.net/10371/123828-
dc.description학위논문 (석사)-- 서울대학교 대학원 : 기계항공공학부, 2015. 2. 김종암.-
dc.description.abstractThe present research focuses on the system preconditioning and the scaling of numerical dissipations of RoeM and AUSMPW+ methods to enable more efficient and accurate computations of all-speed two-phase flows. Previous all-speed two-phase RoeM and AUSMPW+ methods have applied only steady system preconditioning technique while unsteady system preconditioning is essential for the convergence acceleration of unsteady low Mach number flows. In this study, unsteady system preconditioning is achieved by the consideration of Strouhal number in preconditioning parameter. Unlike existing preconditioning techniques, scaling factors in numerical dissipations are treated separately with preconditioning parameter in system so that the numerical instability and the accuracy degradation issues in low Mach number regions are resolved regardless of the convergence. The extension of two-phase RoeM and AUSMPW+ methods to general equation of state (EOS) is completed through the modification of shock discontinuity sensing term (SDST) to be independent on EOS. The performance of the modified SDST is confirmed to be as stable as the previous SDST which works well, but is compatible only with specific forms of EOS.-
dc.description.tableofcontents1.Introduction 1
1.1 Computation of All-speed Two-phase Flows 1
1.2 Thesis Objectives 3
2 Governing Equations 5
2.1 Homogeneous Mixture Equations 5
2.1.1 Two-phase Navier-Stokes Equations 5
2.1.2 Determination of Mixture Properties 7
2.2 Preconditioning Techniques 7
3 Numerical Methods 11
3.1 Extension of Two-phase RoeM and AUSMPW+ to General EOS 11
3.1.1 Original Two-phase All-speed RoeM 12
3.1.2 Original Two-phase All-speed AUSMPW+ 13
3.1.3 Generalization of SDST 15
3.2 System Preconditioning for Unsteady Flows 20
3.3 Scaling of Numerical Dissipations 22
3.3.1 Properly Scaled Two-phase All-speed RoeM 26
3.3.2 Properly Scaled Two-phase All-speed AUSMPW+ 28
4 Numerical Results 30
4.1 Single-phase Flow Computation 31
4.1.1 Steady Inviscid Flow over a NACA0012 Airfoil 31
4.1.2 Steady Viscous Flow over a RAE2822 Airfoil 31
4.1.3 Steady Inviscid Flow around a Cylinder 34
4.1.4 Unsteady Inviscid Vortex Propagation 38
4.2 Two-phase Flow Computation 42
4.2.1 Two-phase Shocktube 42
4.2.2 Shock/Water-Column Interaction 45
4.2.3 Cryogenic cavitation 48
5 Conclusions 50
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dc.formatapplication/pdf-
dc.format.extent5068903 bytes-
dc.format.mediumapplication/pdf-
dc.language.isoen-
dc.publisher서울대학교 대학원-
dc.subjectAll-speed flow-
dc.subjectTwo-phase flow computation-
dc.subjectPreconditioning-
dc.subjectScaling of numerical dissipations-
dc.subjectShock discontinuity sensing term (SDST)-
dc.subjectHomogeneous mixture model-
dc.subject.ddc621-
dc.titleAll-speed Two-phase Computations for General Equation of State with Preconditioning Techniques and Scaling of Numerical Dissipations-
dc.typeThesis-
dc.description.degreeMaster-
dc.citation.pagesvi, 56-
dc.contributor.affiliation공과대학 기계항공공학부-
dc.date.awarded2015-02-
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