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How to simulate boundary conditions and apply uniformly distributed load to shell element when I do nonlinear analysis of I-BEAM

Submitted by speedeagle on

Hi, everyone:

I am using ABAQUS to do my final dissertation:nonlinear analysis of steel members.

When I simulated the beam with shell element, first I define reference points at both end of the beam and assign 'RIGID BODY/PIN OR TIE' to  nodes at the edge,after that I applied bending moments and boundary conditions to both reference points.  But after I finished the buckling analysis, the result is not reasonable,the eigen value is about two times the the value I expected.

Opening for Research Fellow Position in Composite Structures

Submitted by mekchu on

 

July 4, 2011Opening for Research Fellow Position in Composite Structures

The Research Center for Aircraft Parts Technology in Gyeongsang National University (Jinju, South Korea) has opened a postdoctoral research fellow position for the research on composite structures. 

In situ nanocompression testing of irradiated copper

Submitted by Daniel Kiener on

Dear colleagues,

we recently published a paper on measuring bulk properties of irradiated copper from nanoscale samples:

http://www.nature.com/nmat/journal/vaop/ncurrent/full/nmat3055.html

Hope you find this interesting!

 

Daniel

Variables definition in Abaqus

Submitted by Laurianne on

Hi,

I am working on a 3D contact problem where a spherical part is pressed against another spherical surface. I was wondering what variables may be interesting to study for this problem. I decided to look at the contact area CAREA, the contact pressure CPRESS and the stress S but I am not able to find how Abaqus defines and calculates these variables, does anyone know?



Thanks

energy balance of surface-based cohesive of composite under impact in Absqus 6-10

Submitted by moustachiio on

Hi there! I am really new to Abaqus and I need to model a composite
laminated crash cone under impact to a flat solid wall (analytical
surface is used). I modelled a cone with a layers of conventional shell
elements with hashin failure criteria and surface-based cohesive
behaviour as interaction between layers representing the interface of
composite laminates. The model runs successfully but once I checked the
energy balance, the damage dissipation energy from the cohesive, it
turned out to be NEGATIVE (I think this is wrong).

IASS-IACM 2012: 7th International Conference on Computational Mechanics for Spatial Structures, April 2-4, 2012, Sarajevo

Submitted by Adnan_Ibrahimbegovic on

IASS-IACM 2012 WEB PAGE 

 The final announcement, the conference program and detailed information about the IASS-IACM 2012 will be available at the meeting web page:http://www.gf.unsa.ba/iass-iacm-2012/

viscoplastic analysis of lap shear solder joint

Submitted by luvsharma11 on

Hi all,

I am trying to model a solder joint in double lap shear. I am using the Modified Anand's Model. But for some reasons the analysis is not completing and does not gives any errors as well. Since I am new to abaqus, I am not able to solve this. Here is my input file:

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