Fracture, fatigue, failure and damage evolution. proceedings of the 2017 Annual Conference on Experimental and Applied Mechanics / Volume 7 :
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| Meeting name: | Annual Conference on Experimental and Applied Mechanics (17th : 2017 : Indianapolis, Ind.) |
|---|---|
| Imprint: | Cham, Switzerland : Springer, [2018] |
| Description: | 1 online resource (123 pages) |
| Language: | English |
| Series: | Conference Proceedings of the Society for Experimental Mechanics Series Conference proceedings of the Society for Experimental Mechanics series. |
| Subject: | |
| Format: | E-Resource Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/11541579 |
Table of Contents:
- Preface; Contents; 1 Interface Mechanical Strength and Elastic Constants Calculations via Nano Impact and Nanomechanical Raman Spectroscopy; References; 2 Effect of Strain Rate and Interface Chemistry on Failure in Energetic Materials; References; 3 Characterization of Crack Tip Plasticity in IN-617 Using Indentation and Nano-Mechanical Raman Spectroscopy; References; 4 The Two-Way Relationship Between Residual Stress and Fatigue/Fracture; 4.1 Residual Stress Influence on Fatigue and Fracture and Properties; 4.2 Influence of Fracture Concepts on Residual Stress Measurement; References.
- 5 Designing Brittle Fracture Specimens to Investigate Environmentally Assisted Crack Growth5.1 Introduction; 5.2 Finite Element Model; 5.3 FE Model Validation; 5.4 Bi-material Beam Finite Element Model; 5.5 Steady State Cracking in Schott B/Soda-Lime Glass Rectangular Bimaterial Beam; 5.6 Geometry Design for non-constant SIF; 5.7 Conclusion; References; 6 Flexible Energy Harvesting/Storage Structures for Flapping Wing Air Vehicles; 6.1 Introduction; 6.2 Multifunctional Materials Research Related to Flexible Wings for FWAVS; 6.2.1 Integration of Power Systems into Morphing Wings.
- 6.2.2 System Model for Multifunctional Wings in FWAVs6.2.3 Multifunctional System Analysis for Design Optimization; 6.3 Experimental Results for Multifunctional Wings; 6.3.1 Effects of Integrating Power Elements into Wings on System Model Predictions; 6.3.2 Predicted Effects from Integrating Flexible Solar Cells and Batteriesinto Wings for FWAVs; 6.4 Conclusions; References; 7 The Influence of Formulation Variation and Thermal Boundary Conditions on the Near-Resonant Thermomechanics of Mock Explosives; 7.1 Introduction; 7.2 Experimental Techniques; 7.2.1 Sample Preparation.
- 7.2.2 Experimental Setup7.3 Results and Discussion; 7.3.1 Experimental Results; 7.3.1.1 Mechanical Response; 7.3.1.2 Thermal Response; 7.3.2 Thermal Simulation; 7.4 Conclusions; References; 8 Detecting Fatigue Crack Closure and Crack Growth Delays After an Overload Using DIC Measurements; 8.1 Introduction; 8.2 Experimental Details; 8.3 Results and Discussion; 8.4 Conclusion; References; 9 In-Situ Observation of Damage Evolution in Quasi-Isotropic CFRP Laminates; 9.1 Introduction; 9.2 Specimen Preparation; 9.3 Test Setup; 9.4 Results and Discussion; 9.4.1 Global Response.
- 9.4.2 Gradual Development of Damages9.4.3 Interlaminar Shear Strain; 9.5 Summary; References; 10 Contamination-Induced Degradation/Enhancement of Interfacial Toughness and Strength in Polymer-Matrix Composite Interfaces; 10.1 Introduction; 10.2 Experimental Framework; 10.3 Results; 10.4 Conclusions; References; 11 Direct and Simultaneous Extraction of Mixed-Mode Traction-Separation Relations; 11.1 Introduction; 11.2 Experiments; 11.3 Analysis and Results; 11.4 Conclusions; References; 12 Damage Evolution in 304L Stainless Steel Partial Penetration Laser Welds; 12.1 Introduction; 12.2 Methodology.