Dear Fellow Members,
I am currently pursuing my PhD research under the supervision of Prof. Ralf Müller at the Institute for Applied Mechanics, TU Kaiserslautern, Germany. I have submitted my dissertation on October 2014. And expecting to defend my PhD work on March, 2015.
You will be responsible for using numerical methods and computer software to design, develop and validate novel window system. You will also be involved in theoretic analysis and characterisation of conventional noise control design such as microperforated panel (MPPs) and advanced active approaches such as active structural acoustics control. You will also evaluate prototypes and optimising the design until it works by using modelling and simulation as the main tool.
Requirements:
Hi all,
One of our recent works on nanoscale directional motion induced by stiffness gradient.
I hope you will find it interesting.
http://dx.doi.org/10.1103/PhysRevLett.114.015504
This work has been presented in 2014 MRS Spring Meeting by Prof. Huajian Gao (the PPT file he used is attached): https://mrsspring14.zerista.com/event/member/109225
Best,
Tienchong
At the School of Engineering at the University of Glasgow, there is a position open for a Lecturer/Senior Lecturer in the area of Mechanics and Materials (experimental or computational).
Have a look at:
I hope some of you (especially those working on fracture and damage modeling) may find this work interesting:
Modeling damage and fracture within strain-gradient plasticity
http://www.sciencedirect.com/science/article/pii/S0020768315000505#
Hello
I would like to simulate the behavior of an elastomeric ligature used in orthodontic apparatus. I know that its behavior is hyperelastic can anyone hel^p me in the choice of the material property thanks a lot.
I have built shell model of a wind turbine rotor in Abaqus CAE and i have run modal analysis. I see that the first natural frequency is around 1 Hz which is sensible but the displacements are very small 10^-12 which does not make much sense. Max Displacement in the model is always 1 in modal analysis. I am not sure how it is 10^-12 here. Since, the displacements are so small, I cannot increase the scale factor (Exaggerate) for visualization to see where is the problem.
Hi everyone;
I'm trying to simulate FSW plunge state using Abaqus/Explicit, Coupled Eulerian-Lagrangian technique.
As you can see in the picture, NT11, PEV and EVF are calculated. But the problem is that the elements in base metal are not deformed. In other words, the base metal elements which are in contact with PIN remained intact and are not deformed.
Anyone could help me with this?
Following on the previous two webinars on compressor and turbine design for high performance turbochargers, this third and final webinar will highlight the contrasting requirements of high efficiency, high reliability and low manufacturing costs faced by turbocharger manufacturers.
In this session we will highlight how to couple 3D inverse design tools with automatic optimization in order to:
