Doktorarbeit / Dissertation, 2016
292 Seiten
Chapter 1: Introduction
1.1 Overview
1.2 Thesis Objective
1.3 Thesis Outline
1.4 Sandwich Panel Design Concept
1.5 Cellular materials
1.5.1 Stochastic cellular materials
1.5.2 Periodic cellular materials
1.6 Manufacture
1.6.1 Autoclave molding
1.6.2 Filament winding
1.6.3 Resin transfer molding
1.7 Vacuum Assisted Resin Transfer Molding (VARTM) process
1.7.1 Variations of the VARTM process
1.7.2 VARTM process and quality of composite
1.8 Elastic and strength properties of composite materials
1.8.1 Elastic properties of composite materials
1.8.2 Strength properties of composite materials
Chapter 2: Experimental procedures
2.1 Introduction
2.2 Lattice fabrication
2.2.1 Consumable materials
2.2.2 Constituent materials
2.2.3 Preparation Process
2.2.4 Infusion Process
2.2.5 Post infusion process
2.3 Hybrid core sandwich panel studies
2.3.1 Overview
2.3.2 Materials and Manufacturing
2.3.3 Compression tests
2.3.4 Interfacial fracture tests
2.4 Vertical, pyramidal, and octet lattice studies
2.4.1 Overview
2.4.2 Materials and fabrication
2.4.3 Compression tests
2.5 BCC, BCCz, FCC and F2BCC lattice studies
2.5.1 Overview
2.5.2 Materials and fabrication
2.5.3 Compression tests
2.6 Other lattice structures
Chapter 3: Analytical Modeling
3.1 Introduction
3.2 Elastic properties of parent material
3.3 Elastic values
3.4 Strength values
3.5 Analytical model of the compressive response
3.5.1 Analytical predictions for the response of composite pyramidal truss core
3.5.2 Analytical predictions of the vertical column core response
3.5.3 Analytical predictions for the response of the modified pyramidal truss core
3.5.4 Summary
3.5.5 Analytical predictions of the response of the octahedral lattice core
3.5.6 Analytical predictions of the response of the BCC core
3.5.7 Analytical predictions of the response of the FCC core
3.5.8 Analytical predictions of the response of the BCCz core
3.5.9 Analytical predictions of the response of the F2BCC core
Chapter 4: Finite Element Analysis
4.1 Introduction
4.2 ANSYS FE package
4.3 Constitutive models for the composite material
4.3.1 Elastic response
4.3.2 Damage initiation & progression model for the fiber reinforced composites
4.4 Quasi-static Finite element modelling
4.4.1 Modelling of lattice core sandwich structures
4.5 Numerical analysis results
4.5.1 Vertical lattice
4.5.2 Pyramidal lattice
4.5.3 Modified pyramidal lattice
4.5.4 BCC lattice
4.5.5 BCCz lattice
4.5.6 FCC lattice
4.5.7 F2BCC lattice
4.6 Conclusions
Chapter 5: Results and Discussion
5.1 Introduction
5.2 Resin flow and post-manufacture visual assessment
5.2.1 Hybrid GFRP/PET core
5.2.2 Vertical, pyramidal and octet lattice
5.2.3 BCC, BCCz, FCC and F2BCC lattice
5.3 Compression tests
5.3.1 Hybrid GFRP/PET core
5.3.2 Vertical, pyramidal and octet lattice
5.3.3 BCC, BCCz, FCC and F2BCC lattice
5.4 Skin-core Interfacial fracture toughness
5.4.1 Hybrid GFRP/PET core
Chapter 6: Conclusions and Future Work
6.1 Introduction
6.2 Conclusions
6.3 Recommended future work
The primary aim of this research is to investigate the fabrication and mechanical performance of all-composite lattice core sandwich panels. The research focuses on developing a viable lost-mold manufacturing technique to produce these structures, characterizing their mechanical behavior under quasi-static compression, and establishing analytical and finite element models to predict their stiffness and strength.
3.5 Analytical model of the compressive response
The goal of this section is to obtain the elastic properties and collapse strength of the various truss core configurations as a function of the apparent composite material properties and the core geometry. Extensive work has been carried out in developing relations between the parent material properties and the elastic response and the strength prediction of the various lattice core structures [5–11]. The pyramidal core equations included in this chapter serve as an introduction to the topic of deriving elastic and strength response of lattice structures in terms of the parent material properties and geometric properties of the core. This work is further extended to derive similar relations for the vertical column core and the modified pyramidal core.
Chapter 1: Introduction: Discusses the aerospace industry's need for lightweight, high-performance sandwich structures and reviews existing cellular materials and manufacturing methods.
Chapter 2: Experimental procedures: Details the materials, the lost-mold manufacturing process, and the specific test procedures used to measure mechanical properties.
Chapter 3: Analytical Modeling: Derives the mathematical frameworks for predicting the elastic modulus and collapse strength of the various lattice truss core geometries.
Chapter 4: Finite Element Analysis: Provides the methodology and results of numerical simulations performed in ANSYS to validate the analytical models developed in Chapter 3.
Chapter 5: Results and Discussion: Presents the experimental data, including visual assessments, compression tests, and interfacial fracture testing, comparing these results to the analytical and FE predictions.
Chapter 6: Conclusions and Future Work: Summarizes the findings regarding the fabricated lattice structures and suggests potential avenues for future research.
Lattice structures, Sandwich structures, Mechanical properties, Resin infusion, Finite Element, Composites, VARTM, Unidirectional fiber, Compression strength, Micromechanics, Core material, Lost mold technique, Failure mechanisms, Structural efficiency, Energy absorption.
This thesis examines the fabrication, mechanical properties, and predictive modeling of novel all-composite lattice core sandwich panels for aerospace applications.
The study utilizes carbon fiber reinforced plastic (CFRP), glass fiber reinforced plastic (GFRP), and natural jute fibers within epoxy resin matrices.
The goal is to develop a "lost-mold" technique that allows for the creation of complex, free-standing lattice cores that improve mechanical performance and enable better resin infusion.
The research uses both micromechanical analytical models to derive equations for elastic properties and finite element analysis (FEA) via the ANSYS software package for numerical validation.
The research evaluates specific stiffness, compression strength, failure mechanisms, and skin-core interfacial fracture toughness under quasi-static loading conditions.
The fiber volume fraction within the lattice struts is precisely controlled by varying the number of fiber tows inserted during the threading process of the lost-mold technique.
The BCCz lattice is shown to offer superior strength properties and specific energy absorption compared to the standard BCC and octet structures, making it highly effective for energy-absorbing systems.
The wax or salt mold serves as a temporary internal structure that is removed post-curing (by melting or dissolution), resulting in a precise, free-standing composite lattice core.
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