Introduction to nonlinear aeroelasticity
Otros Autores: | |
---|---|
Formato: | Libro electrónico |
Idioma: | Inglés |
Publicado: |
Hoboken, New Jersey ; Chichester, England :
Wiley
2017.
|
Edición: | 1 edition |
Colección: | Aerospace series (Chichester, England)
|
Materias: | |
Ver en Biblioteca Universitat Ramon Llull: | https://discovery.url.edu/permalink/34CSUC_URL/1im36ta/alma991009849089406719 |
Tabla de Contenidos:
- Intro
- Title Page
- Copyright Page
- Contents
- Preface
- Dimitriadis: Nonlinear Aeroelasticity - Series Preface Oct 2016
- About the Companion Website
- Chapter 1 Introduction
- 1.1 Sources of Nonlinearity
- 1.2 Origins of Nonlinear Aeroelasticity
- References
- Chapter 2 Nonlinear Dynamics
- 2.1 Introduction
- 2.2 Ordinary Differential Equations
- 2.3 Linear Systems
- 2.3.1 Stable Oscillatory Response
- 2.3.2 Neutral Oscillatory Response
- 2.3.3 Unstable Oscillatory Response
- 2.3.4 Stable Non-oscillatory Response
- 2.3.5 Unstable Non-oscillatory Response
- 2.3.6 Fixed Point Summary
- 2.4 Nonlinear Systems
- 2.4.1 Linearisation Around Fixed Points
- 2.4.2 The Pitching Wing Section with Cubic Stiffness
- 2.4.3 The Pitchfork Bifurcation
- 2.5 Stability in the Lyapunov Sense
- 2.6 Asymmetric Systems
- 2.6.1 The Fold Bifurcation
- 2.6.2 The Transcritical Bifurcation
- 2.7 Existence of Periodic Solutions
- 2.7.1 Nonlinear Aeroelastic Galloping
- 2.8 Estimating Periodic Solutions
- 2.8.1 Periodic Solutions of the Nonlinear Galloping Oscillator
- 2.8.2 The Hopf Bifurcation
- 2.9 Stability of Periodic Solutions
- 2.9.1 Stability of Galloping Oscillations
- 2.9.3 The Fold Bifurcation of Cycles
- 2.10 Concluding Remarks
- References
- Chapter 3 Time Integration
- 3.1 Introduction
- 3.2 Euler Method
- 3.2.1 Linear Systems
- 3.2.2 Nonlinear Systems
- 3.3 Central Difference Method
- 3.3.1 Explicit Solution of Nonlinear Systems
- 3.3.2 Implicit Solution of Nonlinear Systems
- 3.4 Runge-Kutta Method
- 3.5 Time-Varying Linear Approximation
- 3.6 Integrating Backwards in Time
- 3.7 Time Integration of Systems with Multiple Degrees of Freedom
- 3.8 Forced Response
- 3.9 Harmonic Balance
- 3.9.1 Newton-Raphson
- 3.9.2 Discrete Fourier Transform Techniques
- 3.10 Concluding Remarks
- References.
- Chapter 4 Determining the Vibration Parameters
- 4.1 Introduction
- 4.2 Amplitude and Frequency Determination
- 4.2.1 Event Detection
- 4.3 Equivalent Linearisation
- 4.4 Hilbert Transform
- 4.5 Time-Varying Linear Approximation
- 4.6 Short Time Fourier Transform
- 4.7 Pinpointing Bifurcations
- 4.7.1 Newton-Raphson
- 4.7.2 Successive Bisection
- 4.8 Limit Cycle Study
- 4.9 Poincaré Sections
- 4.10 Stability of Periodic Solutions
- 4.10.1 Floquet Analysis
- 4.11 Concluding Remarks
- References
- Chapter 5 Bifurcations of FundamentalAeroelastic Systems
- 5.1 Introduction
- 5.2 Two-Dimensional Unsteady Pitch-Plunge-ControlWing
- 5.3 Linear Aeroelastic Analysis
- 5.4 Hardening Stiffness
- 5.4.1 Supercritical Hopf Bifurcation
- 5.4.2 Subcritical Hopf Bifurcation
- 5.4.3 Fold Bifurcation of Cycles
- 5.4.4 Flutter of Nonlinear Systems
- 5.4.5 Period-Doubling Bifurcation
- 5.4.6 Torus Bifurcation
- 5.5 Softening Stiffness
- 5.6 Damping Nonlinearity
- 5.6.1 Subcritical Hopf Bifurcation
- 5.6.2 Static Divergence of Cycles
- 5.6.3 Pitchfork Bifurcation of Cycles
- 5.7 Two-Parameter Bifurcations
- 5.7.1 Generalised Hopf Bifurcation
- 5.7.2 Pitchfork-Hopf Bifurcation
- 5.7.3 Hopf-Hopf Bifurcation
- 5.8 Asymmetric Nonlinear Aeroelastic Systems
- 5.8.1 Fold Bifurcation of Fixed Points and Cycles
- 5.8.2 Transcritical Bifurcation of Fixed Points and Cycles
- 5.8.3 Fold-Hopf Bifurcation
- 5.9 Concluding Remarks
- References
- Chapter 6 Discontinuous Nonlinearities
- 6.1 Introduction
- 6.2 Piecewise Linear Stiffness
- 6.2.1 Underlying and Overlying Linear Systems
- 6.2.2 Fixed Points and Boundary Equilibrium Bifurcations
- 6.2.3 Equivalent Linearisation of Piecewise Linear Stiffness
- 6.2.4 Three-Domain Limit Cycles
- 6.2.5 Two-Domain Limit Cycles
- 6.2.6 Time Domain Solutions.
- 6.3 Discontinuity-Induced Bifurcations
- 6.3.1 The Boundary Equilibrium Bifurcation
- 6.3.2 The Grazing Bifurcation
- 6.4 Freeplay and Friction
- 6.5 Concluding Remarks
- References
- Chapter 7 Numerical Continuation
- 7.1 Introduction
- 7.2 Algebraic Problems
- 7.2.1 Prediction Correction
- 7.2.2 Arclength Continuation
- 7.2.3 Pseudo-Arclength Continuation
- 7.3 Direct Location of Folds
- 7.4 Fixed Point Solutions of Dynamic Systems
- 7.4.1 Branch Points
- 7.4.2 Arclength Step Control
- 7.5 Periodic Solutions of Dynamic Systems
- 7.5.1 Starting the Continuation Scheme
- 7.5.2 Folds and Branch Points
- 7.5.3 Branch Switching
- 7.6 Stability of Periodic Solutions Calculated from Numerical Continuation
- 7.7 Shooting
- 7.7.1 Starting the Continuation Scheme
- 7.7.2 Arclength Continuation
- 7.7.3 Stability Analysis
- 7.7.4 Branch Point Location and Branch Switching
- 7.7.5 Grazing
- 7.8 Harmonic Balance
- 7.9 Concluding Remarks
- References
- Chapter 8 Low-Speed AerodynamicNonlinearities
- 8.1 Introduction
- 8.2 Vortex-Induced Vibrations
- 8.3 Galloping
- 8.4 Stall Flutter
- 8.4.1 Dynamic Stall
- 8.4.2 Leishman-Beddoes Model
- 8.4.3 ONERA Model
- 8.4.4 Aeroelastic Simulations using Dynamic Stall Models
- 8.5 Concluding Remarks
- References
- Chapter 9 High-Speed AeroelasticNonlinearities
- 9.1 Introduction
- 9.2 Piston Theory
- 9.3 Panel Flutter
- 9.3.1 Buckling
- 9.3.2 Limit Cycle Oscillations
- 9.4 Concluding Remarks
- References
- Chapter 10 Finite Wings
- 10.1 Introduction
- 10.2 Cantilever Plate in Supersonic Flow
- 10.3 Three-Dimensional Aerodynamic Modelling by the Vortex Lattice Method
- 10.3.1 Aeroelastic Coupling
- 10.3.2 Transforming to the Time Domain
- 10.3.3 Nonlinear Response
- 10.4 Concluding Remarks
- References
- Appendix A Aeroelastic Models
- A.1 Galloping Oscillator.
- A.2 Two-Dimensional Pitch-Plunge-Control Wing Section with Unsteady Aerodynamics
- A.3 Two-Dimensional Pitch-Plunge-Control Wing Section with Quasi-Steady Aerodynamics
- A.4 Two-Dimensional Pitch-Plunge Wing Section with Quasi-Steady Aerodynamics
- A.5 Two-Dimensional Pitching Wing Section with Quasi-Steady Aerodynamics
- A.6 Two-Dimensional Pitch-Plunge Wing with Leishman-Beddoes Aerodynamic Mode
- A.7 Two-Dimensional Pitch-Plunge Wing with ONERA Aerodynamic Model
- A.8 Two-Dimensional Pitch-Plunge-Control Wing Section with Supersonic Aerodynamics
- A.9 Two-Dimensional Pitch-Plunge Wing Section with Supersonic Aerodynamics
- References
- Index.