Hi everyone,
I'm working on a flying wing design for an AeroDesign competition, and I am currently using VSPAero (VLM solver) to extract lateral-directional stability derivatives, specifically Cn_beta and Cy_beta, through a Beta sweep.
I want to add wingtip endplates that extend both upwards and downwards to maximize directional stability. However, when trying to model this, I am running into a few aerodynamic and solver issues:
Mesh Intersections: If I try to model the endplate as a single continuous surface that crosses the wingtip, the solver struggles with the intersecting meshes, resulting in singular matrix errors or unrealistic spikes in the pressure distribution.
Wake Leakage: When using a Fixed Wake, the wake shedding from the main wing cuts directly through the vertical endplate surface. This destroys the pressure gradient and results in a Cn_beta that is near zero.
Reference Area Corruption: If the geometry isn't isolated properly, the solver adds the vertical plate to the reference span (bref) and area (Sref), artificially shrinking the stability coefficients.
To solve this, I am planning to adopt the following setup:
Split the endplate into two separate child geometries attached to the main wing tip.
Set the "Upper Endplate" to a 90-degree dihedral and the "Lower Endplate" to a -90-degree dihedral.
Switch from Fixed Wake to Relaxed Wake (with around 5 iterations) so the wake naturally bypasses the vertical surfaces.
Manually lock the Reference Area and Span to the main wing only.
My question is: Is splitting the endplate into two separate child components and using a Relaxed Wake the official "best practice" in OpenVSP to handle this kind of geometry in VLM? Are there any hidden limitations I should be aware of, or would switching to the Panel Method be strictly necessary for this specific setup?
Thanks in advance for your help and insights!



Hi Rob,
Thank you for the advice. In our current design, the endplate is relatively small compared to the main wing chord. Because of this size proportion, adjusting the endplate chord to cover the wingtip as suggested causes some geometric constraints. Should we proceed using the previous setup where the endplate dimensions are kept as they are without modifying the chords, or is there a specific adjustment recommended for smaller endplates?
