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0 ResultsI have to make a wing for UAV, that material I choose is carbon fiber 230 gpa,have 1000 mm span, 200 mm chord length, NACA 4415 airfoil used , having two spars and 5 ribs, having skin thickness is 1 mm.
by slilbaekslilbaek
lovedeepmehra created this project
about 2 months ago
0 Geometries 0 Meshes 0 Simulation setups 0 ResultsI have to make a wing for UAV, that material I choose is carbon fiber 230 gpa,have 1000 mm span, 200 mm chord length, NACA 4415 airfoil used , having two spars and 5 ribs, having skin thickness is 1 mm.
