Creating a 3D Wing with Pyansys Geometry

[BharathTatavarthi]

I am currently working on a project focused on optimizing the aerodynamic shape of a fixed-wing UAV, and I am using the NACA 2412 airfoil as the reference profile. I am encountering difficulties in creating a 3D wing geometry in PyANSYS Geometry using SpaceClaim Mode. Initially, I attempted to work with a 2D airfoil profile using the PyVista spline command and encountered errors when trying to extrude it.

I am seeking guidance on whether it is possible to create a 3D wing in PyANSYS Geometry with varying chord sections. If it is feasible, could you assist me in understanding how to efficiently create a 3D wing with different chord sections?
my team member @santoshdoddipatla is also asked about this

[RobPasMue]

Hi @Bharath158 - thanks for opening this discussion. I will close it since it is a duplicate of #984. Currently, splines are not supported on PyAnsys Geometry on the Sketch API and thus they cannot be extruded. This depends on features that are not implemented yet on our backend. If there are any updates I will ping you both in #984. Sorry for the inconveniences!

In the meantime you can approximate your spline using straight lines or curves and incrementing the number of points in your spline. I know it is not ideal but it might be a short-term solution.