research
Running MD simulations with LAMMPS
In appendix A of my PhD thesis, I share a MATLAB code to get coordinates of carbon atoms in a graphene sheet. The code also generates the data file required for LAMMPS. In addition, I included a sample input and the corresponding output files from LAMMPS. I hope this will be useful for those who would like to learn MD simulations.
Visual Molecular Dynamics (VMD) package can also be used to obtain coordinates of graphene.
Determination of Density of Laminated Composite
Dear Engineers,
I would like to determine the density of laminated composite which consists of one lamina E-Glass/Epoxy and another one is thin layer of steel plate due to determining Young's Modulus through non-diestructive technique-Impulse excitation.
Any suggestions would be welcome.
var vglnk = { api_url: '//api.viglink.com/api', key: 'a187ca0f52aa99eb8b5c172d5d93c05b' };
var vglnk = { api_url: '//api.viglink.com/api', key: 'a187ca0f52aa99eb8b5c172d5d93c05b' };
Abaqus Subroutine and python subscripting
Dear All,
I was wondering if anyone used abaqus user subroutines to couple the micro and macro models? If any one has used it and is also willing to share the knowledge?
I am looking for some guidance on how to run another *inp and get it's out put in the subroutine. any example on this is greatly appreciated.
Recent paper on the flattening deformation of metal columns
experimental study on lateral compression of square and rectangular metal
columns. Some theoretical relations are derived to predict the absorbed energy,
the specific absorbed energy and the instantaneous lateral load during the
lateral compression. Analytical relations are obtained in two stages: elastic
and plastic parts. In the plastic zone, the total absorbed energy by the column
is calculated, based on the energy method. Then, an analytical equation is
derived to predict the instantaneous lateral load. In the elastic part, the
instantaneous load is obtained by linear behavior assumption. To verify the
Math Kernel Library MKL
Basically, I need to find a few eigenvalues lambda_i and eigenvectors u_i for the problem
KG * u = lambda * KS * u
where KG is the stiffness matrix and KS is the geometric stiffness matrix, also called stress-displacement matrix.
Is KG supposed to be positive definite?
User subroutine UEXPAN
How to use USDFLD request variables from other elements in ABAQUS
Hi all,
Virtual Special Issue: CFD simulation of pedestrian-level wind conditions around buildings: past achievements and prospects
This Virtual Specail Issue deals with papers on CFD simulation of pedestrian-level wind conditions around buildings, published in the Journal of Wind Engineering and Industrial Aerodynamics (JWEIA).
Pagination
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