Evoution of Yield surfaces: Past and Future Trend - Simulation
In continuation of our work on yield surfaces
Part- 1 (node/9016)
Part- 2 (node/9073) and
Part- 3 (node/9103)
Cyclical Nanoindentation Stress-Strain Measurement
The Stress-Strain curve obtained by Nanoindentation reveals the correlation of "Stress" and"Strain" of a given material under nano controlled loads. Unlike the traditional Tensile Testing method of obtaining Stress-Strain curve data, which gives data at a macro level, the Nanoindentation method provides vital Stress-Strain curve data at nano level scale without the large and intense machinery. The Stress-Strain curve of various materials will vary widely.
Design of viscometers corresponding to a universal molecular simulation method
This is the preprint of an article that has appeared in the Journal of Fluid Mechanics, 691:461-486, 2012 (doi:10.1017/jfm.2011.483)
Design of viscometers corresponding to a universal molecular simulation method
by Kaushik Dayal (Carnegie Mellon) and Richard D. James (Minnesota)
Abstract:
On the three-dimensional Filon construct for dislocations
(to appear in the Intl. Journal of Engineering Science)
Robin J. Knops and Amit Acharya
Simulation of fatigue crack growth
Discussion of fracture paper # 2
Advanced Courses on Mechanics of Soft Matter, Zhejiang University, Dec 21-27, 2011
NSFC Advanced Courses on Mechanics of Soft Matter 2011
(Zhejiang University, Dec 21-27, 2011)
CISM Course: Advanced and Bio-Inspired Nanomechanics
Hi all,
There will be a 5 day - course on Advanced and Bio-Inspired Nanomechanics at CISM Udine, Italy.
http://www.cism.it/courses/C1107/
http://media.cism.it/courses%2FC1107%2FPugno4___.pdf
- HG
PS. Original flyer on CISM website:
Advanced and Bio-Inspired Nanomechanics
July 18, 2011 — July 22, 2011
Coordinator:
Linear and non-linear buckling
Hi all,
When we do a non-linear buckling analysis, initially we introduce some imperfections (mode shapes of mode 1, 2 etc) from eigen buckling analysis. Then we multiply the load with eigenvalue of the first mode. This load is applied on the structure having imperfections. Now put on non-linear geometric option and run the analysis. At bifurcation point we get non-linear buckling load. Non-linear buckling load comes close to eigen buckling value.
Decription of my problem is as follows.