benoitpaillard

Hi, the simple plates like 3020 etc... Give non manifold, yet pretty much printable parts. On Thu, Apr 30, 2020, 10:43 AM Chris Eade wrote: > Hello! I noticed on...

Hi all, I'm also interesting in this topic, and I'd like to try and upgrade Cactus to achieve static or dynamic fore-aft tilting. Any information on what's the best approach...

Hi @micheltakken , sorry for the late reply When you import an external file, its unit must be defined in your .export file. Don't hesitate to share your not working...

I'm down ! Can you give me pointers about where that matrix is defined ? I have a couple of test cases at hand to verify the outputs. Cheers !

Hi all, I've tracked down the stiffness matrix definition to these [lines](https://github.com/mdolab/OpenAeroStruct/blob/5c28f3e1d7ff2d2a4e011670530a40da041ecf34/openaerostruct/structures/local_stiff.py#L72-L90) Can anyone confirm that appending this would be enough for the definition of an orthotropic material ?

At first I would like to try and implement something quick and dirty, most likely hard coded, and check the results against our results from [paper](https://www.researchgate.net/publication/348321784_Hydro-elastic_response_of_composite_hydrofoil_with_FSI) I noticed you also...

Still no luck on this one. I cannot find a way to have cmplxfoil accept a secondary aeroproblem... Anyone ? Also if that secondary aeroproblem could be parallelized it would...