Abstract

Lightweight magnesium alloys are being increasingly used in automotive and other transportation industries to achieve energy efficiency. The objective of this thesis was to study the mechanical properties of two wrought alloys AZ31 and AM30. With increasing strain rate the yield strength and ultimate tensile strength increased and the strain hardening exponent decreased for AM30 and increased for AZ31. Both alloys exhibited stable cyclic characteristics at lower strain amplitudes and cyclic hardening characteristics at higher strain amplitudes. The Bauschinger effect was pronounced at higher strain amplitudes, resulting in asymmetric hysteresis loops in both alloys. The influence of strain ratio (Rs), strain rate, and initial straining direction on the cyclic deformation characteristics and fatigue life was evaluated. At low Rs, both alloys exhibited strong cyclic hardening, which decreased as Rs increased. Fatigue crack initiation was observed to occur from the specimen surface and crack propagation was basically characterized by striation-like features.

Highlights

  • Noster and Scholtes [5] mentioned in their work that the strain hardening effect was very small at room temperature; rather, they reported basically the temperature effect on the stress response, while the results presented in this paper showed that, at room temperature, the material could undergo cyclic strain hardening at high strain amplitudes

  • [5] reported in their work on AZ31 extruded alloy that strain hardening effect was very small at room temperature; rather, they reported basically the effect of temperature on the stress amplitude response, while the results presented in this investigation and by some others [6-9, 11, 13] showed that at room temperature, the material could undergo cyclic strain hardening at high strain amplitudes

  • Microstructural examination revealed that both AZ31 and AM30 showed a non uniform grain distribution along the plate thickness

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Summary

CHAPTER I INTRODUCTION

Except for the fact that magnesium alloys have limited formability due to the hexagonal close-packed (HCP) crystal structure, their light weight trait (density: 1.7 gm/cc versus 2.7 gm/cc for aluminum and 7.8 gm/cc for steel), high strength-to-weight ratio and good damping capacity have made these alloys more desirable than conventional structural materials - steels and aluminum alloys [1-4]. The objective of this study is to evaluate the mechanical properties of two wrought Mg alloys, namely, AZ31 and AM30 Both of these alloys were provided by General Motors Research and Development Center. This investigation compares the microstructure, micro-hardness, tensile properties, low cycle fatigue properties, monotonic and cyclic strain hardening exponent and cyclic deformation characteristics of AZ31 and AM30 alloys at different test conditions. Unless the automobile industry embraces its use, magnesium would not become economically viable in other fields [2]

Physical Metallurgy and Properties
Types of Magnesium Alloys
Tensile Properties
Tensile Strength and Ductility
Tensile Fracture Surfaces
Fatigue and Its Characteristics
Low Cycle Fatigue
Cyclic Stress-Strain Curve
Strain Life Equation
Characteristic Feature of Fatigue Fracture Surface
Crack Initiation and Propagation
Metallography
Quantitative Image Analysis
Micro-hardness Tests
Tensile Tests
Fatigue Tests
Cyclic Stress Responses
Cyclic Strain Resistance
Hysteresis Loops and Mean Stress
Change of Elastic Modulus during Cyclic Deformation
Effect of Strain Ratio
Effect of Strain Rate
Effect of Initial Loading Direction
Fractography
Summary
Stress Response during Cyclic Deformation
Cyclic Plastic Deformation and Hysteresis
Change of Modulus of Elasticity during Cyclic Deformation
Fatigue Life and Low Cycle Fatigue Parameters
Conclusions
Findings
Conference presentations
Full Text
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