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 aeroelasticity for conventional rotary wing aircraft, as well as for the newly emerging t
Rotary wing structural dynamics and aeroelasticity
โ Scribed by Richard L Bielawa
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 2006
- Tongue
- English
- Leaves
- 770
- Series
- AIAA education series
- Category
- Library
No coin nor oath required. For personal study only.
โฆ Table of Contents
Content: * Preface to the Second Edition; * Preface to the First Edition; * 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 Stability; * Elastomeric Devices for Rotorcraft; * Blade-Section Properties; * Cross-over Topics; * Concluding Thoughts; * Appendices.
๐ SIMILAR VOLUMES
An ELBS/LPBB edition is available "This text introduces structural dynamics and aeroelasticity, emphasizing conventional aircraft"--"The book deals at an elementary level with aeroelasticity, a study of static and dynamic behavior of structures under the influence of fluid flow. The level of mater
This text provides an introduction to structural dynamics and aeroelasticity, with an emphasis on conventional aircraft. The primary areas considered are structural dynamics, static aeroelasticity, and dynamic aeroelasticity. The structural dynamics material emphasizes vibration, the modal represent
This text provides an introduction to structural dynamics and aeroelasticity, with an emphasis on conventional aircraft. The primary areas considered are structural dynamics, static aeroelasticity, and dynamic aeroelasticity. The structural dynamics material emphasizes vibration, the modal represent
Provides an introduction to structural dynamics and aeroelasticity, with an emphasis on conventional aircraft.