Postdoctoral position with focus in ultrasonics
A postdoctoral position isavailable in the research group led by Dr. Joseph A. Turner in the Departmentof Engineering Mechanics at the University of Nebraska–Lincoln (UNL).
A postdoctoral position isavailable in the research group led by Dr. Joseph A. Turner in the Departmentof Engineering Mechanics at the University of Nebraska–Lincoln (UNL).
Via Physical Review Focus:
What you see is an optical fiber recoiling due to pulse of light flowing through it. The abstract:
Phys. Rev. Lett. 101, 243601 (2008)
Observation of a Push Force on the End Face of a Nanometer Silica Filament Exerted by Outgoing Light
hello ,
i want to model a three layer beam( costrained layer viscoelastic beam)
how can i modell in ansys & how analize the frequency respose...
What is the difference between CP,CERig and RBE3 used in ANSYS, Can anyone please explain clearly
i'm studying M.S(materials science) and i"m interested in knowing how to do a project work in indenting and extracting mechanical properties of materials using ABAQUS software or using MATLAB. suggest any idea thanks a lot in advance. have a nice time.
In fatigue analysis, it is common to use S-N curve from database for spesific material, and some time for spesific way of loading. Is there any way to predict fatigue from direct simulation? For example, giving cyclic loading (10^5 times) and the material will suffer damage and eventually failed. In some FEM codes (MARC, LSDYNA, etc) there is Lemaitre-Chaboche model used to analyze material behavior under low cycle cyclic loading.
Thanks in advance
Chali
we are using shell element for modeling steel tube and i beam. we are not able to create the connection between those two...
Hi all,
I ran a pre-buckling analysis using ABAQUS. I chose nanometer as my length unit. So for the Young's modulus, since my sample has 100 GPa for the Young's modulus, I put 0.0000001 as the value for the Young's modulus under the material property in the ABAQUS.
However, the resulted eigenvalue (~2 nN) was not as what I expected (~2uN). Based on the calculation based on the Euler buckling theory, the critical load should be around 2 uN.
How can I attach the electrodes to the surfaces of the 3-D piezoelectric sensor attached to the 3-D composite plate in ANSYS?