Hi,
I am trying to use OpenVSP for some Aerodynamic estimates and I have found some code on git that integrates the OpenVSP with Python through the API. I have installed the recommended version of Python and OpenVSP as given on the website ( which is
OpenVSP 3.21.2 Win64 requires Python 3.6-x64) and the installation does work. I do have some issues with the tutorial file which I will get to later.
Currently I am trying to use the following files to compute the aerodynamic coefficients over a simple wing planform geometry. I have attached the code and the geometry file. What I am trying to find is the different types of analysis methods that can be passed through to the ExecAnalysis() function which then runs that analysis on OpenVSP. The code initially called VSPAeroSweep as the analysis method, but I found that my system hangs and doesn't go beyond line
> "rid = vsp.ExecAnalysis(analysis_name)"
I even put some time function to find out the time elapsed between the runs but the system never completed the analysis. It would be really helpful if you could help me with understanding this code. Please let me know what I can do to improve the code. I was facing some errors which I was able to resolve based on finding the geometry types and getting the wing ids.
Hope to hear from you soon.
-Hemant