Blade Element Rotor Theory presents an extension of the blade element rotor theory to describe the dynamic properties of helicopter rotors. It focuses on the more precise 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 blade non-uniform properties, the book covers blade twisting, non-rectangular planform shape of a blade, and inhomogeneous airfoil along a 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 dynamic properties. Features: Focuses on a comprehensive description and accurate determination of the rotor aerodynamic properties. Presents more 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.

Book Information
ISBN 9781032283036
Author Pylyp Volodin
Format Hardback
Page Count 184
Imprint Taylor & Francis Ltd
Publisher Taylor & Francis Ltd
Weight(grams) 156g