The Cornell Fracture Group (CFG) has 2 new PhD student positions open on NASA-sponsored projects.
NASA Constellation University Institutes Project: Develop a hierarchical, multi-scale simulator for damage tolerance and durability of advanced composite structures.
NASA Integrated Resilient Aircraft Control Project: Develop a simulation capability to determine residual strength of damaged aircraft structure.
Hi friends,
iam new to this website,
Iam doing research in the area of fatigue analysis using finite element technique for Burnishing process.
Any body worked in this area ?
If so reply....
Bye
The Center for Cellular Mechanics at U of Illinois has recently hosted a week long summer workshop on Cell Mechano Sensitivity (July 30-Aug 3, 2007. The workshop had lectures in the morning an hands on-labs in the aternoons. All the lectures are on the web (with slides and video). They include a large collection of references. The web also has the laboratory protocols for cell culture, cell fixing and staining, single molecule detection, florescence microscopy, and much more. Visit the website:
Please download and read the following materials.
1-1 ABAQUS tutorial for ES 240.pdf
1-2 Learning ABAQUS.pdf
1-3 CAE Example.pdf
Dear Esteemed Researcher,
It is my pleasure to invite you to submit your recent work as a contribution to the special issue on “Bridging of Material Length Scales” for the journal “International Journal of Materials and Structural Integrity” [http://www.inderscience.com/browse/index.php?journalID=162].
Resonance frequency of a cantilever beam is given by
f=(kn/2pi)*sqrt(EI/mL4)
where, kn=3.52 for cantilever, E is Young's Modulus, I is moment of Inertia, m is mass, L is beam length.
The equation is available in Raymond J. Roark and Warren C. Young, “Formulas for Stress and Strain”, McGraw-Hill, Kogakusha, 5th Edition, (1976).
Can any one help me in deriving this. Or any books or websites which deal with this equation.
I am looking at problems of large deformation and large elastic strain in biological materials, using an analytical model that determines the current deformed state in a single step from the original undeformed state. The approach is to propose a strain energy function to allow the calculation of Piola-Kirchhoff 2 stresses which may then be converted to true Cauchy stresses via the usual mapping. Since I initially calculate PK2 stresses, the strain energy function must be a function of Green strain.
I have advance vibration this term and one of our research homework is to find all solutions that have been presented for parabolic forth order PDE. I am looking for some reference for it. Is there anybody know about it?
Hi,
It's the first time I visit here. I find here a wonderful place.
