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UAV Glider Body

UAV Glider Body

grabcad

The final year project's airfoil design by Gowtham and Kumar features a NACA 23018 airfoil with a center chord length of 0.40 and thickness ratio of 18.0%. The model is crafted by Darwin. The wing has a sweep angle of 25 degrees, while the stabilizer YZ and XY have angles of 20° and 75° bend, respectively. The MH60's centerline measurements are 600 mm at 250 mm, 500 mm at 375 mm, and 241 mm at the end.

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