Blade Element Rotor Theory This book presents an extension of the
conventional blade element rotor theory to describe the dynamic
properties of helicopter rotors. The presented theory focuses on
the accurate mathematical determination of the forces and moments
by which a rotor affects its rotorcraft at specified flight
conditions and control positions. Analyzing the impact of a blade's
non-uniform properties, the book covers blade twisting, the
non-rectangular planform shape of a blade, and inhomogeneous
airfoil along the blade. It discusses inhomogeneous induced airflow
around a rotor disc in terms of the blade element rotor theory.
This book also considers the impact of flapping hinge offset on the
rotor's dynamic properties. Features * Focuses on a comprehensive
description and accurate determination of the rotor's aerodynamic
properties * Presents precise helicopter rotor properties with
inhomogeneous aerodynamic properties of rotor blades * Considers
inhomogeneous distribution of induced flow * Discusses a
mathematical model of a main helicopter rotor for a helicopter
flight simulator This book is intended for graduate students and
researchers studying rotor dynamics and helicopter flight dynamics
General
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