OPEN POSITION AT LMS INTERNATIONAL IN THE FIELD OF
ISOGEMOMETRIC BOUNDARY ELEMENT METHOD
BATWOMAN (Basic Acoustics Training - & Workprogram On
Methodologies for Acoustics - Network) is the Initial Training Network
(ITN) No. 605867, funded under the FP7 Marie Curie programme of
the EC. Duration: Sep. 1, 2013 - Aug. 31, 2017.
Topic: Towards zero prototyping in ceramic component design
Hi, everybody,
I am new in modeling of damage initiation and evolution. my job is modeling damage evolution during castingrion deformation which includes two phases: matrix and graphite. Now I developed a 2D plane strain model and trie to model damage evolution. however, when I defined the damage criterion in material propertis under ABAQUS 6.10 and submitted job, the following error occurs:
Hello Everyone,
I have to simulate and find the pressure on the splines in the universal joint. I have to define contact surface and to find a simple method to run analysis on this joint. I am finding it very difficult to select all the surface on every spline. Also, it will make the simulation very big.
Could anyone please help me to find a method or an easy way out. Any kind of suggestions are most welcome.
Regards
Prahel
Hi all,
I am doing microstructure analysis in 3D. To implement anisotropy, i need to give the orientation data. Does anyone know, how to give the orientation in ABAQUS?
The data i have in hand is Euler Angles... Can i give the data manually for four of five grains?
Also, please tell me about the ORIENT subroutine in ABAQUS...
A highly deformable capacitor made of a soft dielectric and two conformal
electrodes can switch between two states discontinuously, by a first-order transition, as the total
charge varies gradually. When the total charge is small, it spreads evenly over the area of the
capacitor, and the capacitor deforms homogeneously. When the total charge is large, it localizes in
a small region of the capacitor, and this region thins down preferentially. The capacitor will
Good mouring, I am using Abaqus to model a antiplane shear loading of a crack in a plate under planestress condition, therefore i have defined the geometry of the problem with thier mechanical properties and loading; i defind a crack i run the analysis i got this following umbarassing errormessages:
Hi everyone,
I am a working on a cube in abaqus. I had to remove some nodes from the face node sets. To be specific edge nodes. I have defined a function in such a way that after removing them what I have is a list of node labels. I am scripting in python. Can anyone help me in extracting nodes back from nodelabels?
Or is there any better way to remove some nodes from nodelist and get the modified nodelist ?
Thanks
