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Strain energy density for a plate under uniform stretch deformation

Can anyone give a definition about strain energy density for a plate? When a plate under a uniform stretch s, some gives an equation like ek=Es2/2(1+μ)(1-2μ), some gives ek=Es2/2. What are the difference of these two definition? Please note both of the cases are for plane stress conditions. If under plane strain conditions, what is the definition for its strain energy density? Thanks for help.

Looking for some references about damage mechanics!

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1Chaboche J L. Une loi diferentielle d’ endommagement de fatigue avec cumulation non linearire.Revue Francaise de Mecanique,1974, 50-51

2Lemaitre J, Plumtree A. Application of damage concepts to predict creep-fatigue failures. Journal of engineering materials and technology. Transactions of ASME. 1979,101:284-292

Look for some references about damage mechanics!

  1Chaboche J L. Une loi diferentielle d’ endommagement de fatigue avec cumulation non linearire.Revue Francaise de Mecanique,1974, 50-51

2Lemaitre J, Plumtree A. Application of damage concepts to predict creep-fatigue failures. Journal of engineering materials and technology. Transactions of ASME. 1979,101:284-292

Thermoelastic Instability Analysis

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Hi, I am new to iMechanica. I am also not sure whether this post is appropriate here or not.

Modal analysis of a Gas turbine matrix burner using ANSYS

Hi, dear friends,

 I am new  to i-mechanica and working for a reaserch institute for steam and Gas turbine in Aachen,Germany. I am doing Modal  analysis of a Gas turbine matrix burner and want to find out the diffrent mode shapes and the frequency. My problem is, I want to impose a temperature field of round about 1800°C which I will extract from CFD results. SO I would be grateful if any one can tell me how can I impose temperature field to get this modes and frequency because this things are influenced by temperature.

Have a nice day 

Thanking you ,

Kidus

Hi,

I am uisng ABAQUS 6.7/Standard to simulate gear pairs (only static). At a moment I am only taking 2D, so I am using plane strain with quad elements. My problem is how to chnage the mesh refinment with respect to the gears postion, specially on the contact area? 

Thank you in advance for any help 

Does the J-integral method for energy release rate require a small displacement assumption?

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As I understand it, there are many geometries for which the j-integral has been found to give useful simplifications when evaluating the energy release rate. Many of these geometries seem to require small displacements. I would like to know if the small displacement requirement is necessary for the contour integral before any simplifications are made or if small displacements are only necessary because the large deformation geometry of some specimens conflicts with those simplifications.

Second law of thermodynamics and Configurational Mechanics

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Hello,

I have been reading up a lot on "Configurational Mechanics" and frankly i came up with a lot of questions. I am not skeptical at all about it, it just that many things are not clear to me.

shirangi's picture

Effect of Residual stresses on the Interfacial Fracture Toughness of polymer/Metal Interface

When a bi-material sample for the characterization of interfacial fracture toughness is manufactured, the sample is not usually stress-free at room temperature. If an interface between a metallic substrate and a polymeric adhesive is considered, there are essentially two sources of residual stresses for a dry sample at room temperature:

abaqus

salut, je veux des docs que m'aide à maitriser le logiciel ABAQUS, est ce vous pouver m'aider,,, merci d'avance

workbench

hi,

i am satish. i am trying to calculate interference stress in interference fit with following dimensions.there is a difference b/w analytical and simulated results. here i am giving dimensions kindly inform to me the values of von misses and pressure at intereference.

shaft od=938.7378, core id=937.8, and core od=1138.2

E=2.1e5,m=.29and coe.of friction=.14

please... help me...

Thanks

satish

 

 

JOURNAL CLUB DEC 1 08: CYBER-ENABLED PREDICTIVE SCIENCE-BASED CONTINUUM MECHANICS FOR MULTISCALE FRACTURE PROCESS DISCOVERY

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The key to developing materials against failure under extreme environments is the understanding of the interplay between the various physical scales present, from the atomic level interactions, to the microstructural composition and the macroscale behavior. The ability to do this requires new methods that can be used to predict macroscale properties accurately based on microstructures and nanostructures without resorting to empiricism.

any theories on the stress wave propagation in concrete?

does anyone know any current theories on the stress wave propagation in a  complex media(such as concrete or rock).(1D sphere wave or complex)

all i see is the simulation with a complex constitutive model. but i think it`s not perfect. 

hope for your help

Faigue Analysis

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Is it possible to carryout fatigue analysis using Msc fatigue for a assembly consisiting Multi Body Dynamics.

This info is needed for my postgraduate thesis work

Seeking Summer Internship Opportunity

I am a second year undergraduate student of IIT Bombay (www.iitb.ac.in).In the coming summer, we are supposed to undertake an internship with an industrial establishment or a research lab of repute, in or out of India.

NANOSHEL

NANOSHEL makes more than 50 types of products, among which the main products are nanotubes, SWCNT´s, MWCNT´s, nanoparticles,. These products are widely used in the fields such as textile industry, ceramics, chemical fiber, plastics, coatings, cosmetics, rubber, electrical and electronic equipments, electric power generation and boiler and so on.

Problem with nominal vs true values

Hi,

 I have cyclic uniaxial compression data of a PU.  When I look at nominal stress vs nominal strain then the relation is clearly nonlinear (increasing stiffnes with increasing  strain).  When I convert to true stress vs true strain I still have a nonlinear relation, however, not as strong and the stiffness decreases with increasing strain.
When I look at true stress vs stretch, however, the relation seems to be almost (I'm only talking about the first loading cycle) linear. Nominal stress vs stretch is still nonlinear. 

Help on ABAQUS UMAT subroutine

I plan to use UMAT to do some simulations on soft tissue. Since I do not have experiences on this, I hope to find some example UMAT code to start with, especially on the thermo-elasto-pelastic models. I searched from google.com, but can not find useful information. Is there any resource on UMAT fortran code for downloading? Thank you very much.

Fatigue

what softwares can be used to predict the fatigue in Multi body dynamics problems

the information is needed for the post graduate thesis work

 

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