About this title: Drawing on his extensive experience as a practicing engineer, designer, educator, and researcher in rotorcraft, the author presents a comprehensive account of the fundamental concepts of structural dynamics and aero-elasticity for conventional rotary wing aircraft, as well as for tilt-rotor and tilt-wing concepts. Intended for use in graduate-level courses and by practicing engineers, the volume covers all of the important topics needed for the complete understanding of rotorcraft structural dynamics and aeroelasticity, including basic analysis tools, rotating beams, gyroscopic phenomena, drive system dynamics, fuselage vibrations, methods for controlling vibrations, dynamic test procedures, stability analysis, mechanical and aeromechanical instabilities of rotors and rotor-pylon assemblies, unsteady aerodynamics and flutter of rotors, and model testing. The second edition provides more up-to-date solution techniques, as well as new material that the author has developed since the first edition. New chapters have been included dealing with elastomeric devices, airfoil sections with an emphasis on composites, "cross-over" topics, and a historical perspective on the subject material. A new appendix has been provided presenting basic material on composites. The text is further enhanced by the inclusion of problems in each chapter.
Table Of Contents
Preface to the Second Edition
Preface to the First Edition
Introduction
Rotary Wing vs Fixed Wing
Methodology
Basic Analytical Techniques
Linear Single-Degree-of-Freedom System
Fourier Methods
Linear Two-Degree-of-Freedom System
Laplace Transform
Structural Damping
Matrices
Vector Calculus
Theorem of Coriolis
Rotating Beams
Basic Equations for Bending
Reference Uniform Blade
Numerical Methods
Approximate Methods
Two-Bladed Rotor
Blade Torsion Dynamics
Coupling Effects
Gyroscopics
Rotational Motion of a Solid Body
Simplified Gyroscope Equation
Precession and Nutation Characteristics
Gyroscopic Characteristics of Rotor Blades
Drive System Dynamics
Shaft Critical Speeds
Torsional Natural Frequencies of Shafting Systems
Special Devices
Fuselage Vibrations
Dynamic Loads
Harmonic Rotor Hub Loads
Nonrotor Sources of Fuselage Excitation
Rotor-Fuselage Interactions
Methods for Vibration Control
Basic Modification Methodology
Modification of Blade Dynamics
Modification of Fuselage Dynamics
Vibration-Suppression Devices
Vibration Test Procedures
Basic Shake Testing
Other Test Objectives
Stability Analysis Methods: Linear Systems
Basic Concepts
Basic Tools for Linear Systems: Constant Coefficients
Linear Multiple-Degree-of-Freedom Systems: Constant Coefficients
Linear Multiple-Degree-of-Freedom Systems: Periodic Coefficients (Floquet Theory)
Nyquist Criterion for Multiple-Degree-of-Freedom Systems
Mechanical and Aeromechanical Instabilities of Rotors
Unsymmetrical Rotor Instability
Quasi-Steady Aerodynamics
Rotor Weaving
Blade Pitch-Flap-Lag Instability
Rotordynamic Instabilities
Mechanical and Aeromechanical Instabilities of Rotor-Pylon Systems
Multiblade Coordinates and Rotor Modes
Rotor-Nacelle Whirl Flutter
Ground Resonance Instability
Air Resonance
Air Mass Dynamics
Unsteady Aerodynamics and Flutter of Rotors
Introduction and Classification
Two-Dimensional Frequency-Domain Theories
Two-Dimensional Arbitrary Motion Theories
Bending-Torsion Flutter
Three-Dimensional Aerodynamic Theories
Dynamic Stall and Stall Flutter
Analysis of Nonlinear Systems
Introduction
Simple Linearization
Transient Solutions Using Numerical Integration
Quasi-Linearization for Explicit Nonlinearities
Numerical Methods for Stability Estimation
Future Directions
Model Rotor Testing for Aeroelastic Stability
Introduction
Scaling Laws
Model Construction Considerations
Instrumentation and Test Procedures
Aeroelastic Considerations for Nonaeroelastic Testing
Elastomeric Devices for Rotorcraft
Introduction
Examples of Elastomeric Devices
Basic Characteristics of Elastomeric Materials
Elastomeric Lead-Lag Dampers
Other Applications of Elastomerics
Blade-Section Properties
Introduction
Generalized Blade Elastic Properties
Beams with Thin-Shell Closed-Cell Construction
Multicell Beams
Total Section Properties
Hygrothermal Effects in Composites
Prismatic Bars
Cross-over Topics
Interactions of the Rotor Drive and Engine/Fuel Control Systems
Aeroelastic Optimization
Concluding Thoughts
Key Historical Milestones
What's on the Horizon?
Appendix A Glossary of Rotorcraft-Related Terms
Appendix B Charts for Blade Frequency Estimation
Appendix C Generalized Frequency-Domain Substructure Synthesis
Appendix D Basic Equations of Motion for Ground Resonance and Air Resonance
Appendix E Composite Materials---Basics
References
Index
Supporting Materials