Non-linear moisture diffusion in concrete-Need some clarification
Hello,
Hello,
Hi,
I want to simulate the deformation of breast under gravity. I
initially have patient's breast images in one position (supine, with
breast falling on the chest). I want to apply gravity loading and
simulate breast image in another position (prone, with breast falling
away from the chest).
I follow the standard path i.e. segment images (supine data),
generate mesh, import the mesh into ABAQUS, apply material properties,
BCs and loads and run the simulation and I get deformed breast mesh
(simulated prone).
This is the preprint of an article that will appear in Acta Materialia (10.1016/j.actamat.2012.07.050).
Influence of Strain on Space Charge Distribution at Ferroelectric Thin-Film Free Surfaces
by Lun Yang and Kaushik Dayal, Carnegie Mellon University
Abstract
hello
this is pavan at present im doing research with modeling of propeller blades inoreder to findout the airfoil points of b-series propeller blades what is the procedure .please provide me the information
i will be very thankful
hi every one
im just early join to this site ,first of all i ask one question :
what is your suggestion for third year student ?
for improving in mechanical engineering...
yours sincerely
BC student,ali asgari
Hi,
i need some help in writing the surface mesh in abaqus. i have a wing model, meshed using hexahedral mesh. now what i want is to write the surface element detail on a file, containing the element number and its neighbouring four nodes. for example
12, 2 3 5 6
here 12 is the element number and 2,3,5 & 6 are the corresponding nodes.
This is the preprint of an article that will appear in Smart Materials and Structures (SMS)
Title: Crack initiation patterns at electrode edges in multilayer ferroelectric actuators
Authors: Amir Abdollahi and Irene Arias, Universitat Politecnica de Catalunya (UPC), Barcelona
Abstract:
Hi,
i need some help in writing the surface mesh in abaqus. i have a wing model, meshed using hexahedral mesh. now what i want is to write the surface element detail on a file, containing the element number and its neighbouring four nodes. for example
12, 2 3 5 6
here 12 is the element number and 2,3,5 & 6 are the corresponding nodes.
Hellow Mechanics
I wender about the limitation of the Navier methode for the solution of the probleme of plate " Why is vailable only for simply supported plates " for wiche raison " mathimathicaly or another thing.........?
thanks
I am new in this forum.I am trying to model Fibre reinfored Polymer
fracture in ABAQUS . But, In website I could not find any example for
that.I have done fracture model for isotropic material such as
Alluminium using Contour Integral.But, for this FRP I am being unable to
model it.What should be my consideration (different from isotropic)
using this contour integral.I want a tensile matrix cracking or
matrix-fibre interface cracking or fibre cracking. Please help me in
this regard.