Rotary wing structural dynamics and aeroelasticity /

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Bielawa, Richard L.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Reston, Va. : American Institute of Aeronautics and Astronautics, ©2006.
Edición:2nd ed.
Colección:AIAA education series.
Temas:
Helicopters > Aerodynamics.
Aeroelasticity.
Hélicoptères > Aérodynamique.
Aéroélasticité.
Aeroelasticity
Helicopters > Aerodynamics
dissertations.
Academic theses
Academic theses.
Thèses et écrits académiques.
Acceso en línea:Texto completo
Tabla de Contenidos:
  • 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

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