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9781402027116

A Modern Course In Aeroelasticity

by ; ; ; ;
  • ISBN13:

    9781402027116

  • ISBN10:

    1402027117

  • Edition: 4th
  • Format: Paperback
  • Copyright: 2004-10-01
  • Publisher: Kluwer Academic Pub
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Summary

In this new edition, the fundamental material on classical linear aeroelasticity has been revised. Also new material has been added describing recent results on the research frontiers dealing with nonlinear aeroelasticity as well as major advances in the modelling of unsteady aerodynamic flows using the methods of computational fluid dynamics and reduced order modeling techniques. New chapters on aeroelasticity in turbomachinery and aeroelasticity and the latter chapters for a more advanced course, a graduate seminar or as a reference source for an entrée to the research literature.

Table of Contents

Preface xvii
Preface to the First Edition xvii
Preface to the Second Edition xix
Preface to the Third Edition xx
Preface to the Fourth Edition xxi
Short Bibliography xxiii
Introduction (Dowell)
1(4)
Static Aeroelasticity (Dowell)
5(48)
Typical Section Model of An Airfoil
5(13)
Typical section model with control surface
10(6)
Typical section model---nonlinear effects
16(2)
One Dimensional Aeroelastic Model of Airfoils
18(8)
Beam-rod representation of large aspect ratio wing
18(4)
Eigenvalue and eigenfunction approach
22(2)
Galerkin's method
24(2)
Rolling of a Straight Wing
26(15)
Integral equation of equilibrium
26(1)
Derivation of equation of equilibrium
27(1)
Calculation of Cαα
28(1)
Sketch of function S(y1,η)
28(2)
Aerodynamic forces (including spanwise induction)
30(2)
Aeroelastic equations of equilibrium and lumped element solution method
32(1)
Divergence
33(1)
Reversal and rolling effectiveness
34(3)
Integral equation eigenvalue problem and the experimental determination of influence functions
37(4)
Two Dimensional Aeroelastic Model of Lifting Surfaces
41(3)
Two dimensional structures---integral representation
41(1)
Two dimensional aerodynamic surfaces---integral representation
42(1)
Solution by matrix-lumped element approach
43(1)
Other Physical Phenomena
44(3)
Fluid flow through a flexible pipe
44(3)
(Low speed) fluid flow over a flexible wall
47(1)
Sweptwing Divergence
47(6)
References for Chapter 2
51(2)
Dynamic Aeroelasticity (Dowell)
53(116)
Hamilton's Principle
54(6)
Single particle
54(2)
Many particles
56(1)
Continuous body
56(1)
Potential energy
56(3)
Nonpotential forces
59(1)
Lagrange's Equations
60(4)
Example---typical section equations of motion
61(3)
Dynamics of the Typical Section Model of An Airfoil
64(23)
Sinusoidal motion
64(3)
Periodic motion
67(1)
Arbitrary motion
67(6)
Random motion
73(8)
Flutter - an introduction to dynamic aeroelastic instability
81(4)
Quasi-steady, aerodynamic theory
85(2)
Aerodynamic Forces
87(10)
Aerodynamic theories available
91(4)
General approximations
95(1)
`Strip theory' approximation
95(1)
`Quasisteady' approximation
95(1)
Slender body or slender (low aspect ratio) wing approximation
96(1)
Solutions to the Aeroelastic Equations of Motion
97(6)
Time domain solutions
98(2)
Frequency domain solutions
100(3)
Representative Results and Computational Considerations
103(25)
Time domain
103(1)
Frequency domain
103(2)
Flutter and gust response classification including parameter trends
105(1)
Flutter
105(16)
Gust response
121(7)
Generalized Equations of Motion for Complex Structures
128(28)
Lagrange's equations and modal methods (Rayleigh-Ritz)
128(1)
Kinetic energy
129(1)
Strain (potential elastic) energy
130(3)
Examples
133(1)
Torsional vibrations of a rod
133(1)
Bending-torsional motion of a beam-rod
134(1)
Natural frequencies and modes-eigenvalues and eigenvectors
135(1)
Evaluation of generalized aerodynamic forces
136(1)
Equations of motion and solution methods
137(2)
Integral equations of equilibrium
139(2)
Natural frequencies and modes
141(2)
Proof of orthogonality
143(1)
Forced motion including aerodynamic forces
144(3)
Examples
147(1)
Rigid wing undergoing translation responding to a gust
147(6)
Wing undergoing translation and spanwise bending
153(2)
Random gusts-solution in the frequency domain
155(1)
Other Fluid-Structural Interaction Phenomena
156(13)
Fluid flow through a flexible pipe: ``firehose'' flutter
156(2)
(High speed) fluid flow over a flexible wall - a simple prototype for plate or panel flutter
158(7)
References for Chapter 3
165(4)
Nonsteady Aerodynamics (Dowell)
169(106)
Basic Fluid Dynamic Equations
169(13)
Conservation of mass
170(1)
Conservation of momentum
171(1)
Irrotational flow, Kelvin's theorem and Bernoulli's equation
172(2)
Derivation of a single equation for velocity potential
174(1)
Small perturbation theory
175(2)
Reduction to classical acoustics
177(1)
Boundary conditions
178(2)
Symmetry and anti-symmetry
180(2)
Supersonic Flow
182(19)
Two-dimensional flow
182(1)
Simple harmonic motion of the airfoil
183(2)
Discussion of inversion
185(2)
Discussion of physical significance of the results
187(2)
Gusts
189(1)
Transient motion
190(1)
Lift, due to airfoil motion
191(1)
Lift, due to atmospheric gust
192(3)
Three dimensional flow
195(6)
Subsonic Flow
201(31)
Derivation of the integral equation by transform methods and solution by collocation
201(3)
An alternative determination of the Kernel Function using Green's Theorem
204(3)
Incompressible, three-dimensional flow
207(4)
Compressible, three-dimensional flow
211(4)
Incompressible, two-dimensional flow
215(3)
Simple harmonic motion of an airfoil
218(6)
Transient motion
224(5)
Evaluation of integrals
229(3)
Representative Numerical Results
232(6)
Transonic Flow
238(37)
References for Chapter 4
270(5)
Stall Flutter (Sisto)
275(24)
Background
275(1)
Analytical formulation
276(2)
Stability and aerodynamic work
278(1)
Bending stall flutter
279(2)
Nonlinear mechanics description
281(1)
Torsional stall flutter
282(3)
General comments
285(3)
Reduced order models
288(1)
Computational stalled flow
289(10)
References for Chapter 5
294(5)
Aeroelasticity in Civil Engineering (Scanlan and Simiu)
299(78)
Vortex-induced Oscillation
301(13)
Vortex shedding
301(4)
Modeling of vortex-induced oscillations
305(1)
Coupled two-degree-of-freedom equations: wake oscillator models
306(4)
Single-degree-of- freedom model of vortex-induced response
310(4)
Galloping
314(13)
Equation of motion of galloping bodies. The Glauert-Den Hartog necessary condition for galloping instability
314(6)
Description of galloping motion
320(1)
Chaotic galloping of two elastically coupled square bars
321(1)
Wake galloping: physical description and analysis
321(6)
Torsional Divergence
327(1)
Flutter and Buffeting in the Presence of Aeroelastic Effects
328(8)
Formulation and analytical solution of the two-dimensional bridge flutter problem in smooth flow
330(4)
Bridge section response to excitation by turbulent wind in the presence of aeroelastic effects
334(2)
Suspension-Span Bridges
336(25)
Wind tunnel testing of suspended-span bridges
336(2)
Torsional divergence analysis for a full bridge
338(2)
Locked-in vortex-induced response
340(10)
Flutter and buffeting of a full-span bridge
350(10)
Reduction of bridge susceptibility to flutter
360(1)
Tall Chimneys and Stacks, and Tall Buildings
361(16)
Tall chimneys and stacks
361(4)
Tall buildings
365(2)
References for Chapter 6
367(10)
Aeroelastic Response of Rotorcraft (Curtiss and Peters)
377(76)
Blade Dynamics
379(24)
Articulated, rigid blade motion
379(11)
Elastic motion of hingeless blades
390(13)
Stall Flutter
403(6)
Rotor-Body Coupling
409(24)
Unsteady Aerodynamics
433(20)
Dynamic inflow
434(6)
Frequency domain
440(1)
Finite-state wake modelling
441(3)
Summary
444(1)
References for Chapter 7
444(9)
Aeroelasticity in Turbomachines (Sisto)
453(38)
Aeroelastic Environment in Turbomachines
454(1)
The Compressor Performance Map
455(5)
Blade Mode Shapes and Materials of Construction
460(2)
Nonsteady Potential Flow in Cascades
462(5)
Compressible Flow
467(4)
Periodically Stalled Flow in Turbomachines
471(4)
Stall Flutter in Turbomachines
475(2)
Choking Flutter
477(2)
Aeroelastic Eigenvalues
479(2)
Recent Trends
481(10)
References for Chapter 8
487(4)
Modeling of Fluid-Structure Interaction (Dowell and Hall)
491(50)
The Range Of Physical Models
491(5)
The classical models
491(3)
The distinction between linear and nonlinear models
494(1)
Computational fluid dynamics models
495(1)
The computational challenge of fluid structure interaction modeling
495(1)
Time-Linearized Models
496(4)
Classical aerodynamic theory
496(1)
Classical hydrodynamic stability theory
497(1)
Parallel shear flow with an inviscid dynamic perturbation
497(1)
General time-linearized analysis
498(2)
Some numerical examples
500(1)
Nonlinear Dynamical Models
500(24)
Harmonic balance method
503(1)
System identification methods
503(1)
Nonlinear reduced-order models
504(1)
Reduced-order models
504(1)
Constructing reduced order models
505(1)
Linear and nonlinear fluid models
506(1)
Eigenmode computational methodology
507(1)
Proper orthogonal decomposition modes
508(1)
Balanced modes
509(1)
Synergy among the modal methods
509(1)
Input/output models
509(2)
Structural, aerodynamic, and aeroelastic modes
511(1)
Representative results
512(1)
The effects of spatial discretization and a finite computational domain
512(4)
The effects of mach number and steady angle of attack: subsonic and transonic flows
516(5)
The effects of viscosity
521(1)
Nonlinear aeroelastic reduced-order models
522(2)
Concluding Remarks
524(17)
References for Chapter 9
529(9)
Appendix: Singular-Value Decomposition, Proper Orthogonal Decomposition, & Balanced Modes
538(3)
Experimental Aeroelasticity (Dowell)
541(10)
Review of Structural Dynamics Experiments
541(2)
Wind Tunnel Experiments
543(2)
Sub-critical flutter testing
543(1)
Approaching the flutter boundary
544(1)
Safety devices
544(1)
Research tests vs. clearance tests
544(1)
Scaling laws
544(1)
Flight Experiments
545(1)
Approaching the flutter boundary
545(1)
When is flight flutter testing required?
545(1)
Excitation
545(1)
Examples of recent flight flutter test programs
546(1)
The Role of Experimentation and Theory in Design
546(5)
References for Chapter 10
548(3)
Nonlinear Aeroelasticity (Dowell, Edwards and Strganac)
551(60)
Introduction
551(1)
Generic Nonlinear Aeroelastic Behavior
552(2)
Flight Experience with Nonlinear Aeroelastic Effects
554(3)
Nonlinear aerodynamic effects
556(1)
Freeplay
556(1)
Geometric structural nonlinearities
557(1)
Physical Sources of Nonlinearities
557(1)
Efficient Computation of Unsteady Aerodynamic Forces: Linear and Nonlinear
558(2)
Correlations of Experiment/Theory and Theory/Theory
560(6)
Aerodynamic forces
560(6)
Flutter Boundaries in Transonic Flow
566(7)
Limit Cycle Oscillations
573(38)
Airfoils with stiffness nonlinearities
573(2)
Nonlinear internal resonance behavior
575(2)
Delta wings with geometrical plate nonlinearities
577(1)
Very high aspect ratio wings with both structural and aerodynamic nonlinearities
578(3)
Nonlinear structural damping
581(1)
Large shock motions and flow separation
581(13)
Abrupt wing stall
594(1)
Uncertainty due to nonlinearity
595(3)
References for Chapter 11
598(13)
Aeroelastic Control (Clark and Cox)
611(64)
Introduction
611(1)
Linear System Theory
612(5)
System interconnections
612(3)
Controllability and observability
615(2)
Aeroelasticity: Aerodynamic Feedback
617(19)
Development of a typical section model
617(2)
Aerodynamic model, 2D
619(3)
Balanced model reduction
622(1)
Combined aeroelastic model
623(4)
Development of a delta wing model
627(3)
Transducer effects
630(3)
Aerodynamic model, 3D
633(1)
Coupled system
634(2)
Open-Loop Design Considerations
636(6)
HSVs and the modal model
637(1)
Optimization strategy
638(3)
Optimization results
641(1)
Control Law Design
642(5)
Control of the typical section model
644(3)
Control of the delta wing model
647(1)
Parameter Varying Models
647(7)
Linear matrix inequalities
648(1)
LMI controller specifications
649(3)
An LMI design for the typical section
652(2)
Experimental Results
654(13)
Typical section experiment
655(1)
LPV system identification
656(2)
Closed-loop results
658(6)
Delta wing experiment
664(3)
Closing Comments
667(8)
References for Chapter 12
669(6)
Modern Analysis for Complex and Nonlinear Unsteady Flows in Turbomachinery (Hall)
675(29)
Linearized Analysis of Unsteady Flows
676(7)
Analysis of Unsteady Flows
683(5)
Harmonic Balance Method
688(11)
Conclusions
699(5)
References for Chapter 13
701(3)
Appendices
704(39)
Appendix A: A Primer For Structural Response To Random Pressure Fluctuations
705(6)
A.1 Introduction
705(1)
A.2 Excitation-Response Relation For The Structure
705(4)
A.3 Sharp Resonance or Low Damping Approximation
709(1)
Nomenclature
710(1)
References for Appendix A
710(1)
Appendix B: Some Example Problems
711(32)
B.1 For Chapter 2
711(13)
B.2 For Section 3.1
724(6)
B.3 For Section 3.3
730(5)
B.4 For Section 3.6
735(3)
B.5 For Section 4.1
738(5)
Index 743

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