How to form a nolinear TD constitutive relation?
A linear constitutive thermodynamic relation between thermodynamic force f and flux v.
v = Mf, where M is the phenomological coefficient.
How to constitute a nonlinear thermodynamic constitutive relation for an unknown system which we expect to exibit nonlinear behaviour?
Openings in Computational Geomechanics and Rock Physics at ExxonMobil
ExxonMobil Research and Engineering Company has immediate openings in Computational Geomechanics and Rock Physics at its Corporate Strategic Research Laboratory in Annandale, NJ.
To be considered, applicants must satisfy the requirements described in the attached flyer and submit a cover letter and resume directly to the ExxonMobil website (www.exxonmobil.com/ex).
ASME Applied Mechanics Division Call for Nominations
Could anyone help on Drucker-Prager model?
I am using exponent Drucker-Prager model at the moment, is there anyone can tell me where the follow exponent D-P eqation comes from originally?
(σ e)(σ e)=λ(σt)(σt)-3(λ-1)σmσt
Where λ= is hydrostatic stress sensitivity parameter and equal to σc/σt, σe is effective stress, σm is hydrostatic stress, σc, σt are stresses under compression and tension, respectively.
I Would like to include failure in my model
I am doing my master thesis on crash simulation of plywood (7 layers-orthotropic material) structures in buses using explicit LS-DYNA FE program. I would like to include failure in my model. Right now I am working on Mat_054_55 (MAT_ENHANCED_COMPOSITE_DAMAGE…..material model from LS-DYNA material library).
Mat_054_55 allows me to get failure by defining anyone of the following parameters,
Simple strategies to produce perfect long range order in self-assembly
In a recent rapid communication (see attached paper), using principles of pattern formation, we expose some simple stategies to reliably produce perfect long range order in self-assembling systems. Most self-assembling systems exhibit short ranged order. This imperfection is detrimental to several practical applications. It is almost always possible to produce perfect patterns in small domain sizes but self-assembly over a larger areal span results in defects.
Composite analysis using SHELL99
I'm trying to model a composite structure with shell 99 element in Ansys.
I set the thickness and material no. in real constant and prepare an orthotropic material property for that. While ploting the result, as I expect to get the stresses among layers different from other points, but the result is a kind of uniform isotropic graph.
I don't know if any setting other than real constant and material property should be done to get a true result or not. and if I'm true then how can I read the true result.
I will appreciate any help.
Postdoctoral position in Computational Solid Mechanics - School Of Mechanical Engineering Purdue University
Mat_54_55 (LS DYNA material model)
I would like to know the difference between Effective Strain, Effective Plastic Strain and Effective Failure Strain.