mkravos

Hi everyone, For my Bachelor's thesis I am currently working on a blended winglet design for a fixed-wing UAV (root chord = 280, halfspan = 750mm, AR = 6.15), but I'm facing some issues with numerical instabilities at the wing-winglet junction and meshing problems with VLM. To aid with inputting the geometry into XFLR5, I developed a custom Python script (image: Python_code) to generate the coordinates for the blending radius and the straight section of the winglet, to ensure a smooth transition...