Blog posts
International Conference on Engineering Coatings: Processes, Control & Applications
A Three days international conference on Engineering Coatings is going to be held in Indian Institute of Technology, Bombay during Feb 9-11,2012
FREQUENCY DOMAIN
hy everyone
Im working on dynamic explicit poblem.i am attemping to obtain frequency domain from time history of strain.
help plz
best regards
Post doc position at Ecoles des Mines de Douai (FRANCE)
POST-DOC POSITION
Title : Experimental and numerical study
of the composite materials fatigue under multiaxial loadings
The Polymers and Composites Technology & Mechanical Engineering
Department of the Ecole des Mines de Douai (France) is currently offering a
postdoctoral fellow position aiming at studying the behavior of composite
materials under multiaxial loadings.
non linear frequency analysis
Hi,
I'm trying to run a frequency analysis of a composite beam with non-linear properties in Abaqus. Is it possible to make use of the non-linear properties in the frequency analysis. If so how can I do it?
Composite beam in this case refers to a combination of steel and concrete.
Any detailed contributions will be appreciated.
Thanks
Shot Peen Hardness With Nanoindentation
The intention of shot peening is ultimately to alter the mechanical properties of a given surface. By hitting the surface with controlled shot the surface will deform plastically. Proper Instrumentation, nanoindentation, will play a vital factor in achieving reliable and intended results.
Basic question regarding composite failure during impact
Hi everyone.. I am doing low velocity impact analysis on graphite/ epoxy
composite plate using abaqus. I have a basic question. During transverse
impact, when does a composite fail? The transverse tensile strength of
my composite is 45 Mpa, transverse compressive strength is 252Mpa,
Longitudinal tensile & compressive strengths are 1520 and 1590 Mpa
respectively. During my analysis, I got the Maximum von mises stress as
2093MPa at the point of impact, but still the failure criterion is not
composite plate using abaqus. I have a basic question. During transverse
impact, when does a composite fail? The transverse tensile strength of
my composite is 45 Mpa, transverse compressive strength is 252Mpa,
Longitudinal tensile & compressive strengths are 1520 and 1590 Mpa
respectively. During my analysis, I got the Maximum von mises stress as
2093MPa at the point of impact, but still the failure criterion is not
Speech of Acceptance of the 2011 Timoshenko Medal by Alan Needleman
Applied Mechanics Division Honors & Awards Banquet, 15 November 2011, Hyatt Regency, Centennial Ballroom A&B, Third Level.
Nonlinear Material Model using ANSYS
I am performing the static analysis on hydraulics component where I am using the nonlinear material properties with multilinear kinematic material model having yield ~150 ksi and ultimate strength ~210 ksi. However I am getting first principal stress as 280 ksi and von Mises(equivalent) stress ~ 240 ksi.
I checked for the directional stresses where I find the stress in axial direction as ~279 ksi.
Whether it is possible to have the stresses above the given material limit (in this case true ultimate strength is 210 ksi).
I checked for the directional stresses where I find the stress in axial direction as ~279 ksi.
Whether it is possible to have the stresses above the given material limit (in this case true ultimate strength is 210 ksi).