Rotary wing structural dynamics and aeroelasticity

Saved in:

Bibliographic Details
Main Author	Bielawa, Richard L.
Format	Electronic eBook
Language	English
Published	Reston, Va. : American Institute of Aeronautics and Astronautics, ©2006.
Edition	2nd ed.
Series	AIAA education series.
Subjects	Helicopters > Aerodynamics. Aeroelasticity. elektronické knihy electronic books
Online Access	Full text
ISBN	9781628701173 162870117X 1600861091 9781600861093 1600862373 9781600862373 1563476983 9781563476983
Physical Description	1 online resource

Cover

Table of Contents:

Cover
Title
Copyright
Foreword
Table of Contents
Preface
Introduction
Basic Analytical Techniques
Rotating Beams
Gyroscopics
Drive System Dynamics
Fuselage Vibrations
Methods for Vibration Control
Vibration Test Procedures
Stability Analysis Methods: Linear Systems
Mechanical and Aeromechanical Instabilities of Rotors
Mechanical and Aeromechanical Instabilities of Rotor-Pylon Systems
Unsteady Aerodynamics and Flutter of Rotors
Analysis of Nonlinear Systems
Model Rotor Testing for Aeroelastic StabilityElastomeric Devices for Rotorcraft
Blade Section Properties
Cross-over Topics
Concluding Thoughts
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 Materialsâ€?Basics
References
Index