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The book addresses computational methods for solving the problem of vibration, response, loads and stability of a helicopter rotor blade modeled as a rotating beam with flap or out-of-plane bending. The focus is on explaining the implementation of the finite element method in the space and time domain for the free vibration, aeroelastic response and stability problems. The use of Floquet analysis for the aeroelastic stability analysis of rotor blades is also shown. The contents of the book will be useful to researchers in aerodynamics and applied mechanics, and will also serve well professionals working in the aerospace industry.
Engineering. --- Fluids. --- Mechanics. --- Mechanics, Applied. --- Aerospace engineering. --- Astronautics. --- Theoretical and Applied Mechanics. --- Fluid- and Aerodynamics. --- Aerospace Technology and Astronautics. --- Rotors (Helicopters) --- Rotational motion (Rigid dynamics) --- Aerodynamics. --- Mechanics, applied. --- Space sciences --- Aeronautics --- Astrodynamics --- Space flight --- Space vehicles --- Applied mechanics --- Engineering, Mechanical --- Engineering mathematics --- Aerodynamics --- Gyrodynamics --- Revolving bodies --- Rotating bodies --- Dynamics, Rigid --- Aeronautical engineering --- Astronautics --- Engineering --- Hydraulics --- Mechanics --- Physics --- Hydrostatics --- Permeability --- Classical mechanics --- Newtonian mechanics --- Dynamics --- Quantum theory
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Exploiting the properties of piezoelectric materials to minimize vibration in rotor-blade actuators, this book demonstrates the potential of smart helicopter rotors to achieve the smoothness of ride associated with jet-engined, fixed-wing aircraft. Vibration control is effected using the concepts of trailing-edge flaps and active-twist. The authors’ optimization-based approach shows the advantage of multiple trailing-edge flaps and algorithms for full-authority control of dual trailing-edge-flap actuators are presented. Hysteresis nonlinearity in piezoelectric stack actuators is highlighted and compensated by use of another algorithm. The idea of response surfaces provides for optimal placement of trailing-edge flaps. The concept of active twist involves the employment of piezoelectrically induced shear actuation in rotating beams. Shear is then demonstrated for a thin-walled aerofoil-section rotor blade under feedback-control vibration minimization. Active twist is shown to be significant in reducing vibration caused by dynamic stall. The exposition of ideas, materials and algorithms in this monograph is supported by extensive reporting of results from numerical simulations of smart helicopter rotors. This monograph will be a valuable source of reference for researchers and engineers with backgrounds in aerospace, mechanical and electrical engineering interested in smart materials and vibration control. Advances in Industrial Control aims to report and encourage the transfer of technology in control engineering. The rapid development of control technology has an impact on all areas of the control discipline. The series offers an opportunity for researchers to present an extended exposition of new work in all aspects of industrial control.
Aeronautics Engineering & Astronautics --- Mechanical Engineering --- Engineering & Applied Sciences --- Rotors (Helicopters) --- Helicopters --- Vibration. --- Copters --- Helicopter rotors --- Rotating aerofoils --- Rotating wings --- Rotors --- Aerofoils --- Aeronautics --- Flying-machines --- Ground-effect machines --- Astronautics. --- Optical materials. --- Aerospace Technology and Astronautics. --- Vibration, Dynamical Systems, Control. --- Optical and Electronic Materials. --- Control and Systems Theory. --- Cycles --- Mechanics --- Sound --- Optics --- Materials --- Space sciences --- Astrodynamics --- Space flight --- Space vehicles --- Aerospace engineering. --- Dynamical systems. --- Dynamics. --- Electronic materials. --- Control engineering. --- Control engineering --- Control equipment --- Control theory --- Engineering instruments --- Automation --- Programmable controllers --- Electronic materials --- Dynamical systems --- Kinetics --- Mathematics --- Mechanics, Analytic --- Force and energy --- Physics --- Statics --- Aeronautical engineering --- Astronautics --- Engineering
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