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2025-02-18

This verification example analyzes the fluid flow around a glider to determine its drag and lift coefficients as a function of the angle of attack. The results are represented in a drag polar graph, while the velocity field analysis establishes the limit angle for laminar flow over the wing profile. A high-fidelity 3D CAD model in STL format is employed with the RWIND 2 module, ensuring precise simulation of aerodynamic behavior and realistic contour rendering. The integrated graphical depiction reinforces the simulation setup and accuracy of the model’s geometry.


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Glider Aerodynamic Performance

You can download this structural model to use it for training purposes or for your projects. However, we do not assume any guarantee or liability for the accuracy or completeness of the model.

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