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| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
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| International Standard Book Number |
9781118488010 |
| Qualifying information |
cloth |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
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| International Standard Book Number |
9781118700433 |
| Qualifying information |
(ePub) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
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| International Standard Book Number |
1118700430 |
| Qualifying information |
(ePub) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
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| International Standard Book Number |
9781118700426 |
| Qualifying information |
(Adobe PDF) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
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| International Standard Book Number |
1118700422 |
| Qualifying information |
(Adobe PDF) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
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| International Standard Book Number |
9781118700440 |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
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| International Standard Book Number |
1118700449 |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
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| International Standard Book Number |
1118488016 |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
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| International Standard Book Number |
9781118488010 |
| 035 ## - SYSTEM CONTROL NUMBER |
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| System control number |
(OCoLC)883836559 |
| Canceled/invalid control number |
(OCoLC)903971074 |
| -- |
(OCoLC)904962025 |
| -- |
(OCoLC)927508711 |
| 041 ## - LANGUAGE CODE |
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| Language code of text/sound track or separate title |
eng |
| 042 ## - AUTHENTICATION CODE |
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| Authentication code |
pcc |
| 050 00 - LIBRARY OF CONGRESS CALL NUMBER |
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| Classification number |
TL574.A37 |
| 072 #7 - SUBJECT CATEGORY CODE |
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| Subject category code |
TEC |
| Subject category code subdivision |
009000 |
| Source |
bisacsh |
| 082 00 - DEWEY DECIMAL CLASSIFICATION NUMBER |
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| Classification number |
629.132/362 |
| Edition number |
23 |
| 100 1# - MAIN ENTRY--PERSONAL NAME |
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| Preferred name for the person |
Wright, Jan R. |
| Authority record control number |
http://id.loc.gov/authorities/names/n2007073845. |
| 245 10 - TITLE STATEMENT |
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| Title |
Introduction to aircraft aeroelasticity and loads / |
| Statement of responsibility, etc |
Jan R. Wright, Jonathan E. Cooper. |
| 250 ## - EDITION STATEMENT |
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| Edition statement |
Second edition. |
| 264 #1 - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
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| Place of publication, distribution, etc |
Chichester, West Sussex, England : |
| Name of publisher, distributor, etc |
Wiley, |
| Date of publication, distribution, etc |
[2014] |
| 300 ## - PHYSICAL DESCRIPTION |
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| Extent |
1 online resource. |
| 336 ## - CONTENT TYPE |
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| Content type term |
text |
| Content type code |
txt |
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rdacontent. |
| 337 ## - MEDIA TYPE |
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| Media type term |
computer |
| Media type code |
c |
| Source |
rdamedia. |
| 338 ## - CARRIER TYPE |
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| Carrier type term |
online resource |
| Carrier type code |
cr |
| Source |
rdacarrier. |
| 490 1# - SERIES STATEMENT |
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| Series statement |
Aerospace series. |
| 504 ## - BIBLIOGRAPHY, ETC. NOTE |
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| Bibliography, etc |
Includes bibliographical references and index. |
| 505 0# - CONTENTS |
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| Formatted contents note |
Table of Contents<br/>Series Preface xxi<br/><br/>Preface to the Second Edition xxiii<br/><br/>Preface to the First Edition xxv<br/><br/>Abbreviations xxix<br/><br/>Introduction 1<br/><br/>PART I BACKGROUND MATERIAL 7<br/><br/>1 Vibration of Single Degree of Freedom Systems 9<br/><br/>1.1 Setting up Equations of Motion for SDoF Systems 9<br/><br/>1.2 Free Vibration of SDoF Systems 11<br/><br/>1.3 Forced Vibration of SDoF Systems 13<br/><br/>1.4 Harmonic Forced Vibration – Frequency Response Functions 14<br/><br/>1.5 Transient/Random Forced Vibration – Time Domain Solution 17<br/><br/>1.6 Transient Forced Vibration – Frequency Domain Solution 21<br/><br/>1.7 Random Forced Vibration – Frequency Domain Solution 23<br/><br/>1.8 Examples 24<br/><br/>2 Vibration of Multiple Degree of Freedom Systems 27<br/><br/>2.1 Setting up Equations of Motion 27<br/><br/>2.2 Undamped Free Vibration 29<br/><br/>2.3 Damped Free Vibration 31<br/><br/>2.4 Transformation to Modal Coordinates 34<br/><br/>2.5 Two-DoF Rigid Aircraft in Heave and Pitch 38<br/><br/>2.6 ‘Free–Free’ Systems 40<br/><br/>2.7 Harmonic Forced Vibration 41<br/><br/>2.8 Transient/Random Forced Vibration – Time Domain Solution 43<br/><br/>2.9 Transient Forced Vibration – Frequency Domain Solution 44<br/><br/>2.10 Random Forced Vibration – Frequency Domain Solution 44<br/><br/>2.11 Examples 45<br/><br/>3 Vibration of Continuous Systems – Assumed Shapes Approach 49<br/><br/>3.1 Continuous Systems 49<br/><br/>3.2 Modelling Continuous Systems 49<br/><br/>3.3 Elastic and Flexural Axes 51<br/><br/>3.4 Rayleigh–Ritz ‘Assumed Shapes’ Method 52<br/><br/>3.5 Generalized Equations of Motion – Basic Approach 53<br/><br/>3.6 Generalized Equations of Motion – Matrix Approach 58<br/><br/>3.7 Generating Whole Aircraft ‘Free–Free’ Modes from ‘Branch’ Modes 61<br/><br/>3.8 Whole Aircraft ‘Free–Free’ Modes 64<br/><br/>3.9 Examples 65<br/><br/>4 Introduction to Steady Aerodynamics 69<br/><br/>4.1 The Standard Atmosphere 69<br/><br/>4.2 Effect of Air Speed on Aerodynamic Characteristics 71<br/><br/>4.3 Flows and Pressures Around a Symmetric Aerofoil 73<br/><br/>4.4 Forces on an Aerofoil 74<br/><br/>4.5 Variation of Lift for an Aerofoil at an Angle of Incidence 76<br/><br/>4.6 Pitching Moment Variation and the Aerodynamic Centre 77<br/><br/>4.7 Lift on a Three-dimensional Wing 78<br/><br/>4.8 Drag on a Three-dimensional Wing 82<br/><br/>4.9 Control Surfaces 83<br/><br/>4.10 Transonic Flows 84<br/><br/>4.11 Examples 85<br/><br/>5 Introduction to Loads 87<br/><br/>5.1 Laws of Motion 88<br/><br/>5.2 D’Alembert’s Principle – Inertia Forces and Couples 90<br/><br/>5.3 External Loads – Applied and Reactive 94<br/><br/>5.4 Free Body Diagrams 95<br/><br/>5.5 Internal Loads 96<br/><br/>5.6 Internal Loads for a Continuous Member 96<br/><br/>5.7 Internal Loads for a Discretized Member 101<br/><br/>5.8 Intercomponent Loads 103<br/><br/>5.9 Obtaining Stresses from Internal Loads – Structural Members with Simple Load Paths 103<br/><br/>5.10 Examples 104<br/><br/>6 Introduction to Control 109<br/><br/>6.1 Open and Closed Loop Systems 109<br/><br/>6.2 Laplace Transforms 110<br/><br/>6.3 Modelling of Open and Closed Loop Systems using Laplace and Frequency Domains 112<br/><br/>6.4 Stability of Systems 114<br/><br/>6.5 PID Control 121<br/><br/>6.6 Examples 122<br/><br/>PART II INTRODUCTION TO AEROELASTICITY AND LOADS 123<br/><br/>7 Static Aeroelasticity – Effect of Wing Flexibility on Lift Distribution and Divergence 125<br/><br/>7.1 Static Aeroelastic Behaviour of a Two-dimensional Rigid Aerofoil with a Torsional Spring Attachment 126<br/><br/>7.2 Static Aeroelastic Behaviour of a Fixed Root Flexible Wing 130<br/><br/>7.3 Effect of Trim on Static Aeroelastic Behaviour 133<br/><br/>7.4 Effect of Wing Sweep on Static Aeroelastic Behaviour 137<br/><br/>7.5 Examples 142<br/><br/>8 Static Aeroelasticity – Effect of Wing Flexibility on Control Effectiveness 143<br/><br/>8.1 Rolling Effectiveness of a Flexible Wing – Fixed Wing Root Case 144<br/><br/>8.2 Rolling Effectiveness of a Flexible Wing – Steady Roll Case 147<br/><br/>8.3 Effect of Spanwise Position of the Control Surface 151<br/><br/>8.4 Full Aircraft Model – Control Effectiveness 152<br/><br/>8.5 Effect of Trim on Reversal Speed 153<br/><br/>8.6 Examples 153<br/><br/>9 Introduction to Unsteady Aerodynamics 155<br/><br/>9.1 Quasi-steady Aerodynamics 156<br/><br/>9.2 Unsteady Aerodynamics related to Motion 156<br/><br/>9.3 Aerodynamic Lift and Moment for an Aerofoil Oscillating Harmonically in Heave and Pitch 161<br/><br/>9.4 Oscillatory Aerodynamic Derivatives 162<br/><br/>9.5 Aerodynamic Damping and Stiffness 163<br/><br/>9.6 Approximation of Unsteady Aerodynamic Terms 164<br/><br/>9.7 Unsteady Aerodynamics related to Gusts 164<br/><br/>9.8 Examples 168<br/><br/>10 Dynamic Aeroelasticity – Flutter 171<br/><br/>10.1 Simplified Unsteady Aerodynamic Model 172<br/><br/>10.2 Binary Aeroelastic Model 173<br/><br/>10.3 General Form of the Aeroelastic Equations 176<br/><br/>10.4 Eigenvalue Solution of the Flutter Equations 176<br/><br/>10.5 Aeroelastic Behaviour of the Binary Model 177<br/><br/>10.6 Aeroelastic Behaviour of a Multiple Mode System 185<br/><br/>10.7 Flutter Speed Prediction for Binary Systems 185<br/><br/>10.8 Divergence of Dynamic Aeroelastic Systems 188<br/><br/>10.9 Inclusion of Unsteady Reduced Frequency Effects 189<br/><br/>10.10 Control Surface Flutter 193<br/><br/>10.11 Whole Aircraft Model – Inclusion of Rigid Body Modes 199<br/><br/>10.12 Flutter in the Transonic Regime 202<br/><br/>10.13 Effect of Non-Linearities – Limit Cycle Oscillations 202<br/><br/>10.14 Examples 204<br/><br/>11 Aeroservoelasticity 207<br/><br/>11.1 Mathematical Modelling of a Simple Aeroelastic System with a Control Surface 208<br/><br/>11.2 Inclusion of Gust Terms 209<br/><br/>11.3 Implementation of a Control System 210<br/><br/>11.4 Determination of Closed Loop System Stability 211<br/><br/>11.5 Gust Response of the Closed Loop System 213<br/><br/>11.6 Inclusion of Control Law Frequency Dependency in Stability Calculations 214<br/><br/>11.7 Response Determination via the Frequency Domain 215<br/><br/>11.8 State Space Modelling 216<br/><br/>11.9 Examples 217<br/><br/>12 Equilibrium Manoeuvres 219<br/><br/>12.1 Equilibrium Manoeuvre – Rigid Aircraft under Normal Acceleration 221<br/><br/>12.2 Manoeuvre Envelope 226<br/><br/>12.3 Equilibrium Manoeuvre – Rigid Aircraft Pitching 227<br/><br/>12.4 Equilibrium Manoeuvre – Flexible Aircraft Pitching 235<br/><br/>12.5 Representation of the Flight Control System (FCS) 250<br/><br/>12.6 Examples 250<br/><br/>13 Dynamic Manoeuvres 253<br/><br/>13.1 Aircraft Axes 255<br/><br/>13.2 Motion Variables 257<br/><br/>13.3 Axes Transformations 257<br/><br/>13.4 Velocity and Acceleration Components for Moving Axes in 2D 259<br/><br/>13.5 Flight Mechanics Equations of Motion for a Rigid Symmetric Aircraft in 2D 262<br/><br/>13.6 Representation of Disturbing Forces and Moments 265<br/><br/>13.7 Modelling the Flexible Aircraft 267<br/><br/>13.8 Solution of Flight Mechanics Equations for the Rigid Aircraft 272<br/><br/>13.9 Dynamic Manoeuvre – Rigid Aircraft in Longitudinal Motion 273<br/><br/>13.10 Dynamic Manoeuvre – Flexible Aircraft Heave/Pitch 279<br/><br/>13.11 General Form of Longitudinal Equations 287<br/><br/>13.12 Dynamic Manoeuvre for Rigid Aircraft in Lateral Motion 288<br/><br/>13.13 Bookcase Manoeuvres for Rigid Aircraft in Lateral Motion 289<br/><br/>13.14 Flight Control System (FCS) 293<br/><br/>13.15 Representation of the Flight Control System (FCS) 295<br/><br/>13.16 Examples 295<br/><br/>14 Gust and Turbulence Encounters 299<br/><br/>14.1 Gusts and Turbulence 300<br/><br/>14.2 Gust Response in the Time Domain 301<br/><br/>14.3 Time Domain Gust Response – Rigid Aircraft in Heave 303<br/><br/>14.4 Time Domain Gust Response – Rigid Aircraft in Heave/Pitch 310<br/><br/>14.5 Time Domain Gust Response – Flexible Aircraft 316<br/><br/>14.6 General Form of Equations in the Time Domain 321<br/><br/>14.7 Turbulence Response in the Frequency Domain 321<br/><br/>14.8 Frequency Domain Turbulence Response – Rigid Aircraft in Heave 324<br/><br/>14.9 Frequency Domain Turbulence Response – Rigid Aircraft in Heave/Pitch 329<br/><br/>14.10 Frequency Domain Turbulence Response – Flexible Aircraft 330<br/><br/>14.11 General Form of Equations in the Frequency Domain 333<br/><br/>14.12 Representation of the Flight Control System (FCS) 334<br/><br/>14.13 Examples 334<br/><br/>15 Ground Manoeuvres 337<br/><br/>15.1 Landing Gear 337<br/><br/>15.2 Taxi, Take-Off and Landing Roll 342<br/><br/>15.3 Landing 351<br/><br/>15.4 Braking 359<br/><br/>15.5 Turning 360<br/><br/>15.6 Shimmy 361<br/><br/>15.7 Representation of the Flight Control System (FCS) 363<br/><br/>15.8 Examples 363<br/><br/>16 Aircraft Internal Loads 367<br/><br/>16.1 Limit and Ultimate Loads 368<br/><br/>16.2 Internal Loads for an Aircraft 368<br/><br/>16.3 General Internal Loads Expressions – Continuous Wing 370<br/><br/>16.4 Effect of Wing-mounted Engines and Landing Gear 372<br/><br/>16.5 Internal Loads – Continuous Flexible Wing 373<br/><br/>16.6 General Internal Loads Expressions – Discretized Wing 379<br/><br/>16.7 Internal Loads – Discretized Fuselage 384<br/><br/>16.8 Internal Loads – Continuous Turbulence Encounter 387<br/><br/>16.9 Loads Generation and Sorting to yield Critical Cases 388<br/><br/>16.10 Aircraft Dimensioning Cases 390<br/><br/>16.11 Stresses derived from Internal Loads – Complex Load Paths 391<br/><br/>16.12 Examples 391<br/><br/>17 Vibration of Continuous Systems – Finite Element Approach 395<br/><br/>17.1 Introduction to the Finite Element Approach 395<br/><br/>17.2 Formulation of the Beam Bending Element 397<br/><br/>17.3 Assembly and Solution for a Beam Structure 401<br/><br/>17.4 Torsion Element 406<br/><br/>17.5 Combined Bending/Torsion Element 407<br/><br/>17.6 Concentrated Mass Element 408<br/><br/>17.7 Stiffness Element 408<br/><br/>17.8 Rigid Body Elements 409<br/><br/>17.9 Other Elements 410<br/><br/>17.10 Comments on Modelling 411<br/><br/>17.11 Examples 413<br/><br/>18 Potential Flow Aerodynamics 415<br/><br/>18.1 Components of Inviscid, Incompressible Flow Analysis 415<br/><br/>18.2 Inclusion of Vorticity 420<br/><br/>18.3 Numerical Steady Aerodynamic Modelling of Thin Two-dimensional Aerofoils 422<br/><br/>18.4 Steady Aerodynamic Modelling of Three-Dimensional Wings using a Panel Method 425<br/><br/>18.5 Unsteady Aerodynamic Modelling of Wings undergoing Harmonic Motion 429<br/><br/>18.6 Aerodynamic Influence Coefficients in Modal Space 432<br/><br/>18.7 Examples 436<br/><br/>19 Coupling of Structural and Aerodynamic Computational Models 437<br/><br/>19.1 Mathematical Modelling – Static Aeroelastic Case 438<br/><br/>19.2 2D Coupled Static Aeroelastic Model – Pitch 439<br/><br/>19.3 2D Coupled Static Aeroelastic Model – Heave/Pitch 440<br/><br/>19.4 3D Coupled Static Aeroelastic Model 441<br/><br/>19.5 Mathematical Modelling – Dynamic Aeroelastic Response 446<br/><br/>19.6 2D Coupled Dynamic Aeroelastic Model – Bending/Torsion 447<br/><br/>19.7 3D Flutter Analysis 448<br/><br/>19.8 Inclusion of Frequency Dependent Aerodynamics for State–Space Modelling – Rational Function Approximation 450<br/><br/>PART III INTRODUCTION TO INDUSTRIAL PRACTICE 455<br/><br/>20 Aircraft Design and Certification 457<br/><br/>20.1 Aeroelastics and Loads in the Aircraft Design Process 457<br/><br/>20.2 Aircraft Certification Process 459<br/><br/>21 Aeroelasticity and Loads Models 465<br/><br/>21.1 Structural Model 465<br/><br/>21.2 Aerodynamic Model 471<br/><br/>21.3 Flight Control System 473<br/><br/>21.4 Other Model Issues 474<br/><br/>21.5 Loads Transformations 474<br/><br/>22 Static Aeroelasticity and Flutter 475<br/><br/>22.1 Static Aeroelasticity 475<br/><br/>22.2 Flutter 478<br/><br/>23 Flight Manoeuvre and Gust/Turbulence Loads 481<br/><br/>23.1 Evaluation of Internal Loads 481<br/><br/>23.2 Equilibrium/Balanced Flight Manoeuvres 481<br/><br/>23.3 Dynamic Flight Manoeuvres 485<br/><br/>23.4 Gusts and Turbulence 489<br/><br/>24 Ground Manoeuvre Loads 495<br/><br/>24.1 Aircraft/Landing Gear Models for Ground Manoeuvres 495<br/><br/>24.2 Landing Gear/Airframe Interface 496<br/><br/>24.3 Ground Manoeuvres – Landing 496<br/><br/>24.4 Ground Manoeuvres – Ground Handling 497<br/><br/>24.5 Loads Processing 498<br/><br/>25 Testing Relevant to Aeroelasticity and Loads 501<br/><br/>25.1 Introduction 501<br/><br/>25.2 Wind Tunnel Tests 501<br/><br/>25.3 Ground Vibration Test 502<br/><br/>25.4 Structural Coupling Test 503<br/><br/>25.5 Flight Simulator Test 504<br/><br/>25.6 Structural Tests 504<br/><br/>25.7 Flight Flutter Test 505<br/><br/>25.8 Flight Loads Validation 507<br/><br/>Appendices 509<br/><br/>A Aircraft Rigid Body Modes 511<br/><br/>B Table of Longitudinal Aerodynamic Derivatives 513<br/><br/>C Aircraft Symmetric Flexible Modes 517<br/><br/>D Model Condensation 527<br/><br/>E Aerodynamic Derivatives in Body Fixed Axes 531<br/><br/>References 535<br/><br/>Index 539 |
| 520 ## - SUMMARY, ETC. |
|---|
| Summary, etc |
Introduction to Aircraft aeroelasticity and Loads, SecondEdition is an updated new edition offering comprehensivecoverage of the main principles of aircraft aeroelasticity andloads. For ease of reference, the book is divided into three partsand begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control, and then goes on to describesimplified models to illustrate aeroelastic behaviour and aircraftresponse and loads for the flexible aircraft before introducingsome more advanced methodologies. Finally, it explains howindustrial certification requirements for aeroelasticity and loadsmay be met and relates these to the earlier theoretical approachesused. Key features of this new edition include: -Uses a unified simple aeroelastic model throughout thebook -Major revisions to chapters on aeroelasticity -Updates and reorganisation of chapters involving FiniteElements -Some reorganisation of loads material -Updates on certification requirements -Accompanied by a website containing a solutions manual, andMATLAB and SIMULINK programs that relate to the modelsused -For instructors who recommend this textbook, a series oflecture slides are also available Introduction to Aircraft aeroelasticity and Loads, SecondEdition is a must-have reference for researchers andpractitioners working in the aeroelasticity and loads fields, andis also an excellent textbook for senior undergraduate and graduatestudents in aerospace engineering. |
| 545 0# - BIOGRAPHICAL OR HISTORICAL DATA |
|---|
| Biographical or historical note |
About the Author<br/>Jan R. Wright<br/>University of Manchester, UK<br/><br/>Jonathan E. Cooper<br/>University of Bristol, UK |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name as entry element |
Aeroelasticity. |
| Authority record control number |
http://id.loc.gov/authorities/subjects/sh85001300. |
| 655 #4 - INDEX TERM--GENRE/FORM |
|---|
| Genre/form data or focus term |
Electronic books. |
| 700 1# - ADDED ENTRY--PERSONAL NAME |
|---|
| Personal name |
Cooper, Jonathan E. |
| Authority record control number |
http://id.loc.gov/authorities/names/n2007073846. |
| 830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE |
|---|
| Uniform title |
Aerospace series (Chichester, England) |
| Authority record control number |
http://id.loc.gov/authorities/names/no2006133963. |
| 856 40 - ELECTRONIC LOCATION AND ACCESS |
|---|
| Uniform Resource Identifier |
https://onlinelibrary.wiley.com/doi/book/10.1002/9781118700440 |
| Link text |
Full text is available at Wiley Online Library Click here to view |
| 942 ## - ADDED ENTRY ELEMENTS |
|---|
| Source of classification or shelving scheme |
|
| Item type |
EBOOK |