Blog posts
Caltech: secrets of the world’s number one university
Good International news on Caltech and engineering. Ares Rosakis, chair of the Division of Engineering and Applied Science,describes Caltech as “a unique species among universities…a very interesting phenomenon”.More can be found in the attachment or at the link below
http://www.timeshighereducation.co.uk/features/caltech-secrets-of-the-w…
instability induced by incoherent twin boundary in nanotwinned copper
1. Strain hardening and softening in nanotwinned Cu:
Nanotwinned Cu foils with about 99% coherent twin boundaries (TBs) among all the boundaries were made. These coherent
TBs, with an average spacing of 25 nm, were engineered approximately parallel to foil surfaces. Low plane-strain deformation
enhances the hardness by refining microstructure and introducing dislocations. High plane-strain deformation results in crystallographic
lattice rotation and reaction between dislocations and coherent TBs, and induces incoherent TBs, thus twin coarsening and
Atomistic and continuum modelling of temperature-dependent fracture of graphene
Abstract
buckling
dear all : Ihave problem in dynamic buckling analysis in abaqus ,I simulated a shell part and put it between two rigid plates and next i put velocity on the one of the rigid plate for buckling-my value of velocity is 8.33e-5 and its very small value .now after the analysis the shell body was not crushed when i increase the value of velocity the crush will occur but i want crush will occur with this velocity and i dont know what do i.please help me.
Call for Abstracts for IMECE 2014: topic 11-13: Nanomaterials for Energy and publish in Journal of Nanotechnology in Engineering
cantilever with end moment
hello Dear friends
I am working on large deflection of cantilevers with total lagrangian approach. my code is converged very well in cantilever with end point load but when I apply end moment the problem does not converged and tangent stiffness matrix became singular. if there is any special note that I ignored. please help me.
Early Bird gets the...... Discount!
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low reynolds number flow over a capsule in fluent
I've been trying to simulate flow conditions at 100 km altitude over a re entry capsule in fluent.
Conditions are
Temperature:
168.7219
K
Density = 0.000000577 Kg/m3
Pressure = 0.0289 N/m2
I tried using laminar and k-w model. The solution does not converge even after 50000 iterations using the density based solver and ideal gas equation.
Is there a way to go about it?
Please let me know.
UPDATED: Nanobrücken 2014 Nanomechanical Testing Workshop
Dear Colleague: You are cordially invited to participate in the Nanobrücken 2014 Nanomechanical Testing Workshop, which will take place March 26-28, 2014 at INM - Leibniz Institute for New Materials in Saarbrücken, Germany. This will be the 4th edition of the annual Nanobrücken workshop series. This year's Keynote Speaker will be Andrew Minor (University of California, Berkeley).