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Robust and Accurate Multi-dimensional Limiting Strategy for Higher-order Methods : 고차 정확도 수치 기법에 적합한 강건하고 정교한 다차원 공간 제한 기법 개발

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dc.contributor.advisor김종암-
dc.contributor.author박진석-
dc.date.accessioned2017-07-13T06:13:30Z-
dc.date.available2017-07-13T06:13:30Z-
dc.date.issued2014-02-
dc.identifier.other000000017649-
dc.identifier.urihttps://hdl.handle.net/10371/118366-
dc.description학위논문 (박사)-- 서울대학교 대학원 : 기계항공공학부, 2014. 2. 김종암.-
dc.description.abstractThe present works deals with a robust and accurate multi-dimensional limiting strategy for higher-order CFD methods to analyze compressible flows. It consists of two parts: extension of multi-dimensional limiting process on unstructured grids and higher-order multi-dimensional limiting strategy.
In first part, the multi-dimensional limiting process (MLP), which has been successfully proposed on structured grids in finite volume method (FVM), is extended to unstructured grids. The basic idea of the MLP limiting strategy is to control the distribution of both cell-averaged and cell-vertex physical properties to mimic multi-dimensional nature of flow physics, which can be formulated to satisfy so called the MLP condition. The MLP condition can guarantee high-order spatial accuracy and improved convergence without yielding spurious oscillations. Starting from the MUSCL-type linear reconstruction on unstructured grids followed by the efficient implementation of the MLP condition, MLP slope limiters on unstructured grids are obtained. Thanks to its superior limiting strategy and maximum principle satisfying characteristics, the proposed MLP on unstructured grids is quite effective in controlling numerical oscillations as well as accurate in capturing multi-dimensional flow features. Examining robust multi-dimensional oscillation control mechanism, it is expected that MLP idea can be extended to higher-order CFD methods.
Based on the MLP on FVM, the second part deals with extension of the MLP limiting philosophy into higher-order CFD methods. In order to enforce monotonicity for higher-order Pn proximation, two concepts are proposed: the augmented MLP condition and P1-projected MLP condition. Both conditions are successfully suppress multi-dimensional oscillations for arbitrary higher-order Pn approximation. Combining extrema detector, based on behavior of local smooth extrema, accurate and robust MLP based troubled-cell markers are developed. For the troubled-cells, the projection procedure and MLP slope limiter adjust sub-cell distributions. This limiting strategy are developed and implemented in the modal discontinuous Galerkin (DG) method and nodal correction procedure via reconstruction (CPR).
Through extensive numerical analyses and computations on unstructured grids, it is demonstrated that the proposed limiting methods for higher-order CFD methods yields outstanding performance in resolving non-compressive as well as compressive flow features.
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dc.description.tableofcontentsAbstract i
Contents iii
List of Figures vii
List of Tables xiii
Chapter 1 Introduction 1
1.1 Higher-order CFD Methods 1
1.2 Limiting Strategy for Higher-order Methods 4
1.3 Objective of the Present research 6
Chapter 2 Governing Equation 7
2.1 Governing Equation of Fluid Dynamics 7
2.1.1 Euler Equations 7
2.1.2 Navier-Stokes Equations 8
2.1.3 Non-dimensionalized Form 9
2.2 Some Model Equations 10
Chapter 3 Numerical Methods for Finite Volume Methods 11
3.1 Spatial Discretization 12
3.1.1 Numerical Flux Functions 12
3.1.2 MUSCL-type Linear Reconstruction 17
3.2 Time Integration 20
3.2.1 Unsteady Computation 20
3.2.2 Implicit Time Integration for Steady Computation 21
Chapter 4 Multi-dimensional Limiting Process on Unstructured Grids 24
4.1 Multi-dimensional Limiting Condition and Maximum Principle . 24
4.2 Formulation of MLP on Unstructured grids 34
4.2.1 MLP-u Slope Limiter 34
4.2.2 Improvement MLP-u2 for Steady State Computation 35
4.2.3 MLP-u Slope Limiters and Conventional Limiters 37
Chapter 5 Numerical Experiments of MLP-u Slope Limiter 50
5.1 Convergence Studies 50
5.1.1 Isentropic Vortex Problem 50
5.1.2 Three-dimensional Compressible Flow with a Sinusoidal Source 54
5.2 Unsteady Computation Results 56
5.2.1 Double Mach Reflection 56
5.2.2 A Mach 3 Wind Tunnel with a Step 58
5.2.3 Shock Tube Problems 59
5.2.4 Three-dimensional Explosion Problems 60
5.2.5 Interaction of Shock Wave with Cone 62
5.2.6 Viscous Shock Tube Problem 65
5.3 Steady Computation Results 68
5.3.1 Transonic Flows around NACA0012 Airfoil 68
5.3.2 Inviscid Flow over a Circular Bump 69
5.3.3 Inviscid Transonic Flow over the ONERA M6 Wing 75
Chapter 6 Higher-order CFD Methods 79
6.1 Discontinuous Galerkin Method 79
6.1.1 Conservation Laws by DG Method 79
6.1.2 Numerical Integration 80
6.1.3 Shape Function and Element Mapping 81
6.1.4 DG Formulation for Navier-Stokes Equations 84
6.2 Correction Procedure via Reconstruction 86
6.2.1 CPR Formulation 86
6.2.2 Element Mapping for Curved boundary 89
6.2.3 CPR Formulation for Navier-Stokes Equations 89
6.3 Time Integration 90
Chapter 7 Multi-dimensional Limiting Strategy for Higher-order CFD Methods 93
7.1 Limiting Issue for Higher-order Methods on Multi-dimensional Flows 93
7.2 Simple MLP-based Troubled-cell Marker 94
7.2.1 Augmented MLP Condition 94
7.2.2 Simple MLP-based Limiting for DG-Pn approximation 96
7.3 Hierarchical MLP limiting for Pn approximation 99
7.3.1 Hierarchical MLP Limiting for DG Method 99
7.3.2 Implementation for CPR Method 103
7.3.3 Experiments for Troubled-cell Marker 104
7.4 P1-projected MLP for Pn approximation 107
7.5 Extension to Euler and Navier-Stokes Equations 114
Chapter 8 Numerical Experiments of MLP on Higher-order CFD Methods 115
8.1 Convergence Studies 116
8.1.1 Euler Equations with Isentropic Vortex Advection 116
8.1.2 Navier-Stokes Equations with a Source Term 116
8.2 Inviscid Flow Computation 118
8.2.1 Shock Tube Problems 118
8.2.2 Double Mach Reflection 124
8.2.3 A Mach 3 Wind Tunnel with a Step 128
8.2.4 Strong Vortex-Shock Wave Interaction 129
8.2.5 Interaction of Shock Wave with 2-D Wedge 130
8.2.6 Interaction of Shock Wave with Circular Density Bubble 134
8.2.7 Interaction of Shock Wave with Spherical Density Bubble 141
8.3 Viscous Flow Computation 141
8.3.1 Oblique Shock Mixing Layer Interaction 141
8.3.2 Three-dimensional Oblique Shock Mixing Layer Interaction 145
Chapter 9 Conclusions 148
9.1 Summary 148
9.2 Future Works 150
국문초록 167
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dc.formatapplication/pdf-
dc.format.extent45868091 bytes-
dc.format.mediumapplication/pdf-
dc.language.isoen-
dc.publisher서울대학교 대학원-
dc.subjectHigh-speed compressible flow-
dc.subjectMulti-dimensional limiting process-
dc.subjectHigher-order CFD methods-
dc.subjectDiscontinuous Galerkin method-
dc.subjectCorrection procedure via reconstruction-
dc.subjectUnstructured grids-
dc.subject.ddc621-
dc.titleRobust and Accurate Multi-dimensional Limiting Strategy for Higher-order Methods-
dc.title.alternative고차 정확도 수치 기법에 적합한 강건하고 정교한 다차원 공간 제한 기법 개발-
dc.typeThesis-
dc.contributor.AlternativeAuthorPark, Jin Seok-
dc.description.degreeDoctor-
dc.citation.pagesxiv, 168-
dc.contributor.affiliation공과대학 기계항공공학부-
dc.date.awarded2014-02-
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