Hi Steve and Rob
I've been using OpenVSP, NASTRAN95 (the open source one) and pyNastran for a while now on an ultralight sailplane design. I'm excited to see what you two, working together, might accomplish!
I'm happy to offer up help, advice, opinions, or testing where I can. I've written a few scripts but but I'm not a programmer by any stretch of imagination. I was a aero/structures analyst by trade.
My current "workflow" is pretty bad from "flow" point of view:
I figured out my aircraft configuration mostly with OpenVSP.
I create NASTRAN95 models of components by hand (old school use
of spreadsheets and text, or simple scripts to generate the grids
and elements, then I'll either assume pressure distributions or
use XFLR5 to get panel by panel data to map using a custom python
script to the PLOAD4 cards.
I can confirm the quality/look of the FEM mesh by changing the
.inp file extension to .bdf . I then have to start pyNastranGUI
from a command line with the file as an argument. (I don't know
why it wont work if I start the gui then point it to the file. but
it doesn't)
Then I run the analysis with the .inp file using NASTRAN95.
There is a DMAP alter to get NASTRAN95 to output an OP2 file.
Once the .bdf is up in the gui I can then read in the .op2
results. It gets the displacements OK, but it doesn't translate
the cquad4 stress results for some reason. I can use a python
script to get those stress results in a .csv file that I CAN read
into pyNastranGUI and display and there it is...results!
So I have a work around for each hurdle but...getting meshes and
mapped loads out of OpenVSP, (tweaking the .inp by hand for all
the properties, materials, and boundary conditions is fine by me)
then running them in NASTRAN95, and viewing results in
pyNastranGUI. That would be awesome!
-Peter Hudson-
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