Numerical simulation of a quadrotor blade based on structure effect at staticthrust conditions
Drone propellers are rotating wings producing lift in the direction of the axis of rotation.
Propeller blade design is critical to generate enough thrust to carry the takeoff weight and reduce
aerodynamics noise level. In this project, numerical analysis is conducted for the aerodynamics
performance of two propeller designs at the static thrust condition. ... ادامه مطلب