Hypersonic Fluid Structure Interaction with openFoam?
this is my first message in this forum, so I first say Hi to everyone here!
My question is: I have written my final thesis (university degree) about a transient fluid structure interaction of the hypersonic flight of a rocket with ANSYS CFX. The heating of the structure (rocket nose) has also been studied. I now want to model the same problem with openFoam.
Do you know if that is possible?
I found a solver named areafoam. Is this suitable for this? Do you now other solvers? Do I need more than one solver?
Do you know if aerofoam works with the newest release of openfoam (v2.1.1)?
I have just started using openFoam, so I am not very familiar with that yet.
Hope you can give me some help!
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