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2 Geometries
5 Meshes
1 Simulation setup
7 ResultsFlying-wing delta UAV, 1700 mm span, LE sweep 52.2 deg, symmetric 12% section. Incompressible steady RANS, k-omega SST, alpha sweep 0/4/8/12 deg at 25 m/s. S_ref 1.479 m2, L_ref 0.985 m (MAC).
by slilbaekslilbaek
vhusak created this project
about 1 month ago
2 Geometries 5 Meshes 1 Simulation setup 7 ResultsFlying-wing delta UAV, 1700 mm span, LE sweep 52.2 deg, symmetric 12% section. Incompressible steady RANS, k-omega SST, alpha sweep 0/4/8/12 deg at 25 m/s. S_ref 1.479 m2, L_ref 0.985 m (MAC).
