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Soft Materials Mechanics and the 2017 ASME IMECE

Submitted by mechanics.soft… on

Dear Colleagues,

The Soft Materials Mechanics Technical Committee (TC) is pleased to announce that the abstract submission process for the 2017 ASME IMECE in Tampa, FL is open. The TC symposium solicits abstracts from many disciplines represented from previous years (active materials, gels, biomaterials, 3D printing, and more) as well new subject areas and collaborations.

Issues with implementation of strain gradient plasticity framework of Niordson and Hutchinson (2003) in Abaqus UEL subroutine

Submitted by Suman.Guha on

I have implemented the rate-independent strain gradient plasticity framework of Niordson and Hutchinson (2003) in UEL. I was able to validate the results of the shear of infinitely wide thin layer between two rigid surfaces (Niordson and Hutchinson, 2003). However, the UEL subroutine fails to converge for the more complex problem of the shear of finite width slab. I suspect the convergence issues are arising out of internal elastic-plastic boundary conditions and the yield criteria. I have few doubts in this regard.

 

Issues with the implementation of Strain gradient plasticity framework of Niordson and Hutchinson (2003) in ABAQUS UEL

Submitted by Suman.Guha on

I have implemented the rate-independent strain gradient plasticity framework of Niordson and Hutchinson (2003) in UEL. I was able to validate the results of the shear of infinitely wide thin layer between two rigid surfaces (Niordson and Hutchinson, 2003). However, the UEL subroutine fails to converge for the more complex problem of the shear of finite width slab. I suspect the convergence issues are arising out of internal elastic-plastic boundary conditions and the yield criteria. I have few doubts in this regard.

 

Is there any dissymetry of lift in the forward flight of the helicopter after applying the cyclic control?

Submitted by seepratik on

Dear friends,

I was curious about the time varying loads on the helicopter blades in the forward flight. After reaching lots of books and documents, I came to know that some control (cyclic) is applied to take care of the dissymetry of lift in the forward flight. My question is, if the dissymetry of lift is eliminated by applying the cyclic control or by blade flapping (whatever), then why the load should vary with time for the 90 and 270 position of the blade? Can anybody explain this? Please let me know the justification. I am really curious about it. 

Thanks

Call for Abstract Submission to the USNCCM14: Modeling Materials with Coupled Physics

Submitted by sergkuznet on

Dear Colleagues:

The 14th U.S. National Congress on Computational Mechanics (USNCCM14) will be held at the Palais des Congrès de Montréal, QC, Canada,  July 17-20, 2017 (http://14.usnccm.org/).

As a part of this meeting, we are organizing a mini-symposium to address recent advances in Modeling Materials with Coupled Physics (http://14.usnccm.org/MS709). Topics of particular interest include (but not limited to)

“Deflecting elastic prism” and unidirectional localisation for waves in chiral elastic systems

Submitted by Giorgio Carta on

For the first time, a design of a “deflecting elastic prism” is proposed and implemented for waves in a chiral medium. A novel model of an elastic lattice connected to a non-uniform system of gyroscopic spinners is designed to create a unidirectional wave pattern, which can be diverted by modifying the arrangement of the spinners within the medium.

MIT Multiscale Materials Design Course 2017 / June 12-16, 2017

Submitted by Markus J. Buehler on

Spend a week at MIT and earn a MIT certificate. A great opportunity for postdocs and graduate students. Limited number of fellowships available. 

June 12-16, 2017

URL: http://professional.mit.edu/programs/short-programs/multiscale-materials-design