Please find attached a report on a comparison between ANSYS SHELL181 and SOLSH190 elements with particular emphasis on applicability to linear elastic sandwich panels.
Title: Comparison of Ansys elements Shell181 and Solsh190
Abstract:
Applicants are sought to fill a post-doctoral position in
computational solid/structural mechanics and design. The selected applicant will work
closely with Prof. Masoud Rais-Rohani and his research colleagues and graduate
students at the Center for Advanced Vehicular Systems (CAVS) in the Bagley
College of Engineering at Mississippi State University. Applicants must have strong background
in finite element analysis with good knowledge of commercial codes such as ABAQUS, LS-DYNA, or MD Nastran.
Applicants are sought to fill a post-doctoral position in
computational solid/structural mechanics and design. The selected applicant will work
closely with Prof. Masoud Rais-Rohani and his research colleagues and graduate
Have you ever seen a structure subject to flutter instability?
Can flutter instability be connected to dry friction?
We provide positive answers to the above questions, watch the video at
Hi, for my project, using ANSYS i have to build a model of RCC frame on soil. I want to analyse the effect of soil-structure interaction. Can anyone help me in these regard. My e-mail id is ayon_buet [at] yahoo.com. I would be very happy, if i got some pdf files of modeling soil-structure type problems.......
Dear Colleagues,
We are going to demonstrate the possibilities of IOSO Design Optimization Software. Very quick video shots. Just take a glance at it.
Optimization of 3D serpentine cooling passage in turbine blade. 42 design
variables in total.
Hi
I was trying to find the brillouin zone of a GaAs superlattice and their points of symmetry to use it in determing the bandstructure. I am using the [111] as the z direction and the structure is periodic in the x and y direction but none periodic in the z direction. I am still looking for my way in this field and i couldnt find a good textbook that explain this, especially how to find the symmetry points of a crystal whether it is in bulk stucture or superlattice. So i really would appreciate any help or guidance in this problem.
Hello,
i am using Abaqus/Standard to simulate the contact of a ball with a flat. Up to this point the simulation is no problem and gives good results compared to the herzian theory. But within my bachelor thesis i have to add a coat (with layers) to the flat (Thickness: 0.004 mm) and analyse the influence of the coat material to the stresses. My idea is to create a skin on the plate and a shell composite section. Then i assign the skin to this section. In the field output i defined the section points to get the stresses over the thickness of the shell.
