Publications

Detailed Information

Viscoelastic analysis of multilayered composite structures based on higher-order zigzag theory : 고차 지그재그 이론을 이용한 복합재료 적층 구조물의 점탄성 거동 해석

DC Field Value Language
dc.contributor.advisorMaenghyo Cho-
dc.contributor.author누엔시녁-
dc.date.accessioned2018-11-12T01:01:37Z-
dc.date.available2018-11-12T01:01:37Z-
dc.date.issued2018-08-
dc.identifier.other000000153121-
dc.identifier.urihttps://hdl.handle.net/10371/143331-
dc.description학위논문 (박사)-- 서울대학교 대학원 : 공과대학 기계항공공학부, 2018. 8. Maenghyo Cho.-
dc.description.abstractThis dissertation investigates the viscoelastic behaviors of multilayered composite structures based on efficient higher-order zigzag theory. In addition, the coupling hygrothermal-mechanical problem also is analyzed considering how the viscoelastic properties of material depending on the temperature and moisture of environments. Moreover, the analysis of delamination growth in the viscoelastic laminate in the creep process is examined. The efficient higher order zigzag theory given in the thesis has their own advantages such as:

(1) It is accurate for both global and local responses by superimposing linear zigzag field on a varying cubic displacement fields.

(2) It requires only five number of unknown variables which is independent of layer number. Therefore, it is very potential to analyze thick laminates with hundreds of layers.

(3) It can be easy to reduce to other simpler theories such as classical laminated theory, first-order shear deformation theory and third-order shear deformation theory which all are well known.

In this study, the time-dependent relaxation moduli of composite materials have the form of Prony series, which can be determined by the master curve from experimental data. The constitutive equation of linear viscoelastic materials in the form of the Boltzmann superposition integral is simplified by the convolution theorem of the Laplace transform to avoid direct integration as well as to improve both computational accuracy and efficiency. By using the equivalent linear elastic stress-strain relationship in the corresponding Laplace domain, the transverse shear stress-free conditions at the top and bottom surfaces and the transverse shear stress continuity conditions at the interfaces between layers are satisfied conveniently. Thus, the structures and advantages of the EHOPT can be preserved in viscoelastic laminated composites in the Laplace domain.

For finite element analysis, since the time dimension is transformed to Laplace domain, the finite element discretization is only used in the spatial domain. A nonconforming three-node triangular element is employed to implement the viscoelastic EHOPT. To pass the proper bending and shear patch tests in arbitrary mesh configurations, the modified shape function developed by Specht is applied and converted into Laplace domain. Therefore, the final numerical results, which is obtained by using inverse Laplace techniques, always converge to the corresponding analytical solutions.

For coupling hygrothermal-mechanical problem, the temperature and moisture fields are also assumed in the form of efficient higher-order theory and calculated by solving continuity condition at the interface and employing the thermal and hygroscopic variation principle.

In order to verify the efficiency and accuracy of the present study, some numerical examples for long-term creep and relaxation processed are performed. The present study provides a powerful tool to accurately investigate the responses of the viscoelastic or time-dependent mechanical behaviors of multilayered composite structures
-
dc.description.tableofcontentsABSTRACT 2

TABLE OF CONTENTS 4

LIST OF FIGURES 7

LIST OF TABLES 10

CHAPTER 0. INTRODUCTION 12

0.1. Short Review of Multilayered Plate and Shell Theories 12

0.2. Viscoelastic Behaviors of Multilayered Composite 13

0.3. Research Content and Organization 15

CHAPTER 1. VISCOELASTICITY 17

1.1. Constitutive Equation for Viscoelastic Materials 17

1.2. Inverse Laplace Transform 18

CHAPTER 2. HIGHER-ORDER ZIGZAG THEORY FOR PLATE MODEL 20

2.1. Formulation for Higher-Order Zigzag Plate Theory 20

2.2. Formulation for Finite Element Method 24

2.3. Numerical Results of Plate Models 28

2.3.1. Inverse Laplace transform comparison 32

2.3.2. Creep process 34

2.3.3. Relaxation process 38

2.4. Numerical Results of Finite Element Models 41

2.4.1. Rate of convergence 43

2.4.2. Creep process 44

2.4.3. Relaxation process 56

CHAPTER 3. HIGHER-ORDER ZIGZAG THEORY FOR SHELL MODEL 61

3.1. Preliminary background of Naghdis shell model 61

3.2. Formulation for Higher-Order Zigzag Shell Theory 63

3.3. Numerical Results 68

3.3.1. Elastic comparison 69

3.3.2. Viscoelastic behaviors 70

CHAPTER 4. COUPLING HYGROTHERMAL-MECHANICAL PROBLEM 80

4.1. Constitutive Equation for Hygrothermal-Viscoelastic Materials 80

4.2. Temperature and Moisture Conductitity Analysis 81

4.3. Hygrothermal-Mechanical Coupled Problem for Plate Model 84

4.4. Numerical Results 88

4.4.1. Hygrothermal distribution through the thickness 89

4.4.2. Viscoelastic behaviors 93

CHAPTER 5. CONCLUDING REMARK 96

APPENDIX 98

Appendix 1: Tranverse shear stress condition for plate models 98

Appendix 2: Component of the stiffness matrix K* for plate models 100

Appendix 3: Transverse shear stress condition for shell models 100

Appendix 4: Component of the stiffness matrix K* for shell models 102

Appendix 5: Transverse shear stress condition for plate model under hygrothermal-mechanical loading 103

Appendix 6: Component of the K* and F* in the governing equation 106

REFERENCES 109
-
dc.language.isoen-
dc.publisher서울대학교 대학원-
dc.subject.ddc621-
dc.titleViscoelastic analysis of multilayered composite structures based on higher-order zigzag theory-
dc.title.alternative고차 지그재그 이론을 이용한 복합재료 적층 구조물의 점탄성 거동 해석-
dc.typeThesis-
dc.contributor.AlternativeAuthorNguyen Sy Ngoc-
dc.description.degreeDoctor-
dc.contributor.affiliation공과대학 기계항공공학부-
dc.date.awarded2018-08-
Appears in Collections:
Files in This Item:

Altmetrics

Item View & Download Count

  • mendeley

Items in S-Space are protected by copyright, with all rights reserved, unless otherwise indicated.

Share