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Stable, non-Reflective Condition of Perfectly Matched Layer in Computational Aeroacoustics : 전산공력음향학에서 Perfectly Matched Layer의 안정적인 흡수조건에 관한 연구

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dc.contributor.advisor이수갑-
dc.contributor.author정한아침-
dc.date.accessioned2017-07-14T03:39:06Z-
dc.date.available2017-07-14T03:39:06Z-
dc.date.issued2016-02-
dc.identifier.other000000132104-
dc.identifier.urihttps://hdl.handle.net/10371/123858-
dc.description학위논문 (석사)-- 서울대학교 대학원 : 기계항공공학부 우주항공공학전공, 2016. 2. 이수갑.-
dc.description.abstractIn Computational Aeroacoustics, non-reflective boundary conditions such as radiation or absorbing boundary conditions are critical issues in that they can affect the whole solutions of computation. Among these types of boundary conditions, Perfectly Matched Layer boundary condition which has been widely used in Computational Electromagnetics and Computational Aeroacoustics is developed by augmenting the additional term by an absorption function in the original governing equations so as to stably absorb the outgoing waves. Even if Perfectly Matched Layer is perfectly non-reflective boundary condition analytically, spurious waves at the interface or instability could be shown since the analysis is performed in the discretized space. Hence, the study is focused on factors that affect these numerical instability and accuracy with particular numerical schemes. First, stability analysis preserving the dispersion relation is carried out in order to achieve the stability limit of time-step size. Then, through mathematical approach, stable absorption coefficient and PML width are suggested. In order to validate the prediction of analysis condition, numerical simulations are performed in generalized coordinate system as well as Cartesian coordinate system.-
dc.description.tableofcontentsChapter 1. Introduction 1
1.1 BACKGROUND 1
1.2 MOTIVATION 2
1.3 SCOPE OF PRESENT STUDY 3

Chapter 2. Governing Equations 5
2.1 LINEARIZED EULER EQUATIONS 5
2.2 DERIVATION OF PML EQUATIONS 6
2.2.1 Complex Change of Variables 6
2.2.2 Space-time Transformation 7
2.2.3 Stable PML Equations 9

Chapter 3. Numerical methodology 14
3.1 OPTIMIZED NUMERICAL METHOD 14
3.1.1 Fourier Analysis of High-order Spatial Discretization 14
3.1.2 Optimized Time Discretization Scheme 17
3.2 NUMERICAL STABILITY ANALYSIS 19

Chapter 4. Non-Reflective PML Conditions 24
4.1 END CONDITION OF PML BOUNDARY 24
4.2 ANALYTICAL APPROACH ON ABSORPTION COEFFICIENT 28
4.2.1 Maximum Absorption Coefficient 28
4.2.2 Minimum Absorption Coefficient 34

Chapter 5. Numerical Tests 38
5.1 STABILITY ANALYSIS RESULTS 39
5.1.1 Sound Propagating in Low Mach number Uniform Flow 40
5.1.2 Sound Propagating in High Mach number Uniform Flow 40
5.2 ACCURACY ANALYSIS RESULTS 42
5.2.1 Sound Propagating in Cartesian Grid System 42
5.2.2 Sound Propagating in Curvilinear Grid System 44

Chapter 6. Concluding Remarks 51

References 52

Abstract in Korean 56
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dc.formatapplication/pdf-
dc.format.extent5272682 bytes-
dc.format.mediumapplication/pdf-
dc.language.isoen-
dc.publisher서울대학교 대학원-
dc.subjectHigh-order Finite Difference-
dc.subjectDispersion-Relation-
dc.subjectStability Analysis-
dc.subjectComputational Aeroacoustics-
dc.subjectPerfectly Matched Layer-
dc.subject.ddc621-
dc.titleStable, non-Reflective Condition of Perfectly Matched Layer in Computational Aeroacoustics-
dc.title.alternative전산공력음향학에서 Perfectly Matched Layer의 안정적인 흡수조건에 관한 연구-
dc.typeThesis-
dc.contributor.AlternativeAuthorChoung Han Ah Chim-
dc.description.degreeMaster-
dc.citation.pages68-
dc.contributor.affiliation공과대학 기계항공공학부-
dc.date.awarded2016-02-
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