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The Rotating Beam Problem in Helicopter Dynamics

  • Ranjan Ganguli
  • Vijay Panchore

Part of the Foundations of Engineering Mechanics book series (FOUNDATIONS)

Table of contents

  1. Front Matter
    Pages i-xiii
  2. Ranjan Ganguli, Vijay Panchore
    Pages 1-39
  3. Ranjan Ganguli, Vijay Panchore
    Pages 41-60
  4. Ranjan Ganguli, Vijay Panchore
    Pages 61-81
  5. Ranjan Ganguli, Vijay Panchore
    Pages 83-91
  6. Ranjan Ganguli, Vijay Panchore
    Pages 93-97
  7. Back Matter
    Pages 99-99

About this book

Introduction

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.

Keywords

Finite element method in space Helicopter flapping blade Computational method Finite element method in time Aeroelastic stability

Authors and affiliations

  • Ranjan Ganguli
    • 1
  • Vijay Panchore
    • 2
  1. 1.Department of Aerospace EngineeringIndian Institute of ScienceBangaloreIndia
  2. 2.Department of Aerospace EngineeringIndian Institute of ScienceBangaloreIndia

Bibliographic information

  • DOI https://doi.org/10.1007/978-981-10-6098-4
  • Copyright Information Springer Nature Singapore Pte Ltd. 2018
  • Publisher Name Springer, Singapore
  • eBook Packages Engineering
  • Print ISBN 978-981-10-6097-7
  • Online ISBN 978-981-10-6098-4
  • Series Print ISSN 1612-1384
  • Series Online ISSN 1860-6237
  • Buy this book on publisher's site
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