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Titlebook: Experimental and Applied Mechanics, Volume 4; Proceedings of the 2 Carlos E. Ventura,Wendy C. Crone,Cosme Furlong Conference proceedings 20

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书目名称Experimental and Applied Mechanics, Volume 4
副标题Proceedings of the 2
编辑Carlos E. Ventura,Wendy C. Crone,Cosme Furlong
视频video
概述This is the fourth volume in the Proceedings of the 2012 Annual Conference on Experimental and Applied Mechanics.Includes supplementary material:
丛书名称Conference Proceedings of the Society for Experimental Mechanics Series
图书封面Titlebook: Experimental and Applied Mechanics, Volume 4; Proceedings of the 2 Carlos E. Ventura,Wendy C. Crone,Cosme Furlong Conference proceedings 20
描述.Experimental and Applied Mechanics, Volume 4: Proceedings of the 2012 Annual Conference on Experimental and Applied Mechanics., the fourth volume of seven from the Conference, brings together 54 contributions to this important area of research and engineering. The collection presents early findings and case studies on fundamental and applied aspects of Experimental and Applied Mechanics, including papers on: .Fracture & Fatigue.Microscale & Microstructural Effects in Fatigue & Fracture.Material Applications.Composite Characterization Using Digital Image Correlation Techniques.Multi-Scale Simulation and Testing of Composites.Residual Stress.Inverse Problems/Hybrid Methods.Nano-Composites.Microstructure Material Characterization.Modeling and Uncertainty Quantification.Impact Behavior of Composites.
出版日期Conference proceedings 2013
关键词Digital Image Correlation; Fracture and Fatigue; Impact Behavior of Composites; Microscale Effects; Micr
版次1
doihttps://doi.org/10.1007/978-1-4614-4226-4
isbn_softcover978-1-4899-9583-4
isbn_ebook978-1-4614-4226-4Series ISSN 2191-5644 Series E-ISSN 2191-5652
issn_series 2191-5644
copyrightThe Society for Experimental Mechanics, Inc. 2013
The information of publication is updating

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,MEMS Device for Fatigue Testing of 25 μm Thick Aluminum Specimens,trength and the longest at stresses near half that value. The cracks exhibited a very abrupt transition from the incubation stage, marked by increasing surface deformations and other evidence of local microstructural damage, to the rapid growth stage. The failure criterion used for the S-N curve was
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High Confidence Level Calibration for AFM Based Fracture Testing of Nanobeams,nt results. A new set of experiments are underway in which the tests are performed by adapting a direct, traceable method for calibrating the AFM cantilever stiffness (Ying ZC et al., Rev Sci Instrum 78:063708, 2007). The improved calibration should not only improve the accuracy of the strength resu
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Measurement of Metallic Adhesion Force-to-Elongation Profile Under High Separation-Rate Conditions,he experiment realized through the Transferred Momentum Measurement Facility reproduces the injection of the LISA TM into geodesic, aiming at quantifying the residual velocity of the mass after separation from the release tip. In the field of dynamic behaviour of materials, the TM injection constitu
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Prediction of Constraint Parameters Along the 3D Crack Front Under Negative Biaxial Loadings,analysis. Some aircraft components operate under negative biaxial loadings up to −0.5. In this work, attempts have been made to quantify the effect of in-plane and out-of-plane constraints along the 3D crack front under different biaxial loadings using elastic–plastic FE analysis approach for AA2014
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Stress Intensity Factors for Viscoelastic Axisymmetric Problems Applied to Wood,ned with an incremental viscoelastic formulation in the time domain. Using a Compact Tension Shear (CTS) specimen, the evolutions of stress intensity factor versus time are posted in each fracture mode configuration. The obtained results demonstrate the efficiency of the proposed model.
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Experimental, Numerical and Analytical Evaluation of Structural Integrity of Experiment Container Swn, 2-g’s lateral, and 2-g’s up were imposed on the container. Analytical models (NASA-required design codes) were used to calculated margins of safety from forces and stresses. Numerical modeling (FEA) was used to determine stresses overall and at critical hotspots. Experimental methods were used t
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