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A single drone propeller is simulated with both 3 and 4 blades configuration. The main goal is to understand the aerodynamic effect of the number of blades, angles of attack and rotational speed. Incompressible steady state solver is used with k-omega turbulence model.
by slilbaekslilbaek
Bjoern_Lau createdthis project
over 8 years ago
jvilar copied this project
over 6 years ago