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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書目名稱Experimental and Applied Mechanics, Volume 4影響因子(影響力)




書目名稱Experimental and Applied Mechanics, Volume 4影響因子(影響力)學(xué)科排名




書目名稱Experimental and Applied Mechanics, Volume 4網(wǎng)絡(luò)公開度




書目名稱Experimental and Applied Mechanics, Volume 4網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱Experimental and Applied Mechanics, Volume 4被引頻次




書目名稱Experimental and Applied Mechanics, Volume 4被引頻次學(xué)科排名




書目名稱Experimental and Applied Mechanics, Volume 4年度引用




書目名稱Experimental and Applied Mechanics, Volume 4年度引用學(xué)科排名




書目名稱Experimental and Applied Mechanics, Volume 4讀者反饋




書目名稱Experimental and Applied Mechanics, Volume 4讀者反饋學(xué)科排名

Traumatic-Grief

西瓜

沒收

,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

DEMN

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

大笑

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.

外來(lái)

Lobotomy

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