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Leishman organizes the complex physics of rotary-wing flight into a logical, multi-part academic progression that balances foundational theories with advanced, modern engineering problems: This public link is valid for 7 days
While excellent for estimating ideal hovering performance, it assumes an infinite number of blades and ignores profile losses, tip vortices, and non-uniform airflow. 2. Blade Element Theory (BET) This public link is valid for 7 days