CFD Based Aeroelasticity
Can anyone provide some guidelines regarding CFD based aeroelasticity? And if possible some references as well.
Can anyone provide some guidelines regarding CFD based aeroelasticity? And if possible some references as well.
Question About Ansys
Hello everyone,
When you create the model (for example a rectangle sample) in abaqus, I don't understand how you apply a crack and how you have a stress distribution in all the sample. Can somebody advise me ?
Thanks in advance.
Infinity.
Hi
Can everybody explain me about "eigensolver , eigenfrequency , eigenmode , eigenvalue , ..."?
Thanks in advance
Ho1mo
CMIS09
5th Contact Mechanics International Symposium
April 28-30, 2009, Chania, Greece
organized by
Prof. G.E. Stavroulakis
Technical University of Crete
Hi
Can every body explain me about "eigenvalue , eigensolver , eigenfrequensy , eigenmode"?
Thanks in Advanced
Ho1mo
HI Every Body
I am postgraduate student of NavalArchitecture, My thesis is Fatigue Crack Propagation in ship Industry, I want to use Ansys Software for this purpose, at first I generated a plate with a central Crack and did fine mesh around crack and saw the results, for next step I should propagate the crack, my questions are as below:
1. How we can predict the Crack path?
2. how should I growth the crack? shall I clear mesh and extend the crack or.....???? I don't know?
3. How Can I use from Interface Elements?
Extended deadline for abstract submission: 31 October
&
Confirmed invited speakers
Hello everyone
I wrote some codes with umat recently . They can work well with single CPU. However, the results become very bad for several CPUs.
I define a matrix with COMMON BLOCK and it seems that COMMON BLOCK can not be used for parallel computing. Are there any ways to resolve this problem?
I am not familiar with fortran.Someone told me that the matrix should be defined by MODULE. I don't know about this.
Please give some helps to me
regards,
Wang