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Scientific Programmer

Submitted by tonycallands on

Global Strategies Group is looking for a Scientific Programmer to design, develop and implement software environment/components for geometry representation and mesh generation in support of computational mechanics applications

 

Significant software development/programming activity is expected.

 

Qualifications:

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Masters or PhD in Engineering or Computer Science

 

Background and experience:

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IV ECCOMAS Thematic Conference, Smart Structures and Materials (SMART’09), 13-15 July 2009, Porto, Portugal

Submitted by Cesar Vasques on

The Faculty of Engineering of the University of Porto (FEUP), with the support of ECCOMAS, invites you to participate in the fourth edition of the international conference Smart Structures and Materials (SMART’09), that will be held at the Campus of FEUP, at the city of Porto, Portugal, from July 13-15, 2009 (www.fe.up.pt/~smart09).

C Clamp

Submitted by saravanan.venkatesh on

hello sir

                I am saravana,doing M.E,I am doing a project on C Clamp which has a hole at its centre,generally there are two C Clamp at right angles to each other,when one of the c clamp is modelled and rotated to make the other one at 90 degree,the centre of two clamp is not coinciding.so Please give me some suggestion

Mechanics of Microtubules Buckling Supported by Cytoplasm

Submitted by Hanqing Jiang on

The cytoskeleton provides the mechanical scaffold and maintains the integrity of cells.  It is usually believed that one type of cytoskeleton biopolymer, microtubules, bear compressive force.  In vitro experiments found that isolated microtubules may form an Euler buckling pattern with a long wavelength for very small compressive force.  This, however, does not agree with in vivo experiments where microtubules buckle with short-wavelength.  In order to understand the structural role of microtubules in vivo, we (Jiaping Zhang and Hanqing Jiang) developed a mechanics model to study microtubule buckling supported by cytoplasm.  We found that the ability for a cell to sustain compressive force does not solely rely on mic

A Finite Element Method for Transient Analysis of Concurrent Large Deformation and Mass Transport in Gels

Submitted by Hanqing Jiang on

A gel is an aggregate of polymers and solvent molecules.  The polymers crosslink into a three-dimensional network by strong chemical bonds, and enable the gel to retain its shape after a large deformation.  The solvent molecules, however, interact among themselves and with the network by weak physical bonds, and enable the gel to be a conduit of mass transport.  The time-dependent concurrent process of large deformation and mass transport is studied by developing a finite element method. 

Viscoelastic properties

Submitted by Mamilla Ravi Sankar on

Hi I am new to this blog as well as new to Viscoelasticity.  I have some basic quiries on viscoelasticity...as I am beginner to this area.

I am working on a polymer viscoelastic fluid filled with abrasive (Silicon carbide particles) for finishing of metal surfaces.This composition (polymer viscoelastic fluid + abrasive particles) placed in a cylinder and pushed through the hollow cylinderical workpiece with certain extrusion pressure excerted by piston. Due to piston pressure, the abrasives in the composition will abrade the workpiece surface. 

Buckling of thin walled cylindrical shell

Submitted by Himayat Ullah on

I am analyzing a steel thin walled cylidrical shell subjected to axial compression against buckling.I performed both eigen value linear and nonlinear buckling analyses using ANSYS.The buckling load is less than the material yield limit and is therefore elastic buckling.

One of my colleague argues that the shell will regain its original shape after the buckling load is removed,as its is elastic buckling.My plea is that the shell has passed the limit point (buckling load) and it is global buckling and no shape recovery will occur after the load removal.

Ansys Shell181

Submitted by maajidchishti on

Hi All

I am trying to use Shell181 elements to model carbon/epoxy unidirectional composites. When tried to use anisotropic material model ansys wants me to enter coefficients D11 to D21. I am not sure how to calculate the value of these coefficients or where to get their value from. Some help in this regard will be much appreciated. Thank you

Regards

Maajid