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1 Geometry
3 Meshes
1 Simulation setup
3 ResultsExternal aerodynamics CFD of Horangnabi fuselage option C (hybrid) to compute drag coefficient at 13 m/s, AoA 0 deg.
by slilbaekslilbaek
leegunwoo2002 created this project
24 days ago
1 Geometry 3 Meshes 1 Simulation setup 3 ResultsExternal aerodynamics CFD of Horangnabi fuselage option C (hybrid) to compute drag coefficient at 13 m/s, AoA 0 deg.
