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E-raamat: Aerodynamics for Engineers

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  • Formaat: PDF+DRM
  • Ilmumisaeg: 12-Aug-2021
  • Kirjastus: Cambridge University Press
  • Keel: eng
  • ISBN-13: 9781009115957
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Aerodynamics for EngineersSuurem pilt
  • Formaat: PDF+DRM
  • Ilmumisaeg: 12-Aug-2021
  • Kirjastus: Cambridge University Press
  • Keel: eng
  • ISBN-13: 9781009115957
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Now reissued by Cambridge University Press, this sixth edition covers the fundamentals of aerodynamics using clear explanations and real-world examples. Aerodynamics concept boxes throughout showcase real-world applications, chapter objectives provide readers with a better understanding of the goal of each chapter and highlight the key 'take-home' concepts, and example problems aid understanding of how to apply core concepts. Coverage also includes the importance of aerodynamics to aircraft performance, applications of potential flow theory to aerodynamics, high-lift military airfoils, subsonic compressible transformations, and the distinguishing characteristics of hypersonic flow. Supported online by a solutions manual for instructors, MATLAB® files for example problems, and lecture slides for most chapters, this is an ideal textbook for undergraduates taking introductory courses in aerodynamics, and for graduates taking preparatory courses in aerodynamics before progressing to more advanced study.

Muu info

Now reissued by Cambridge University Press, this sixth edition covers fundamental aerodynamics using examples, applications and exercises.
Preface xi
Chapter 1 Why Study Aerodynamics? 1(32)
1.1 Aerodynamics And The Energy-Maneuverability Technique
2(6)
1.2 Solving For The Aerothermodynamic Parameters
8(18)
1.3 Description Of An Airplane
26(1)
1.4 Summary
27(1)
Problems
28(4)
References
32(1)
Chapter 2 Fundamentals Of Fluid Mechanics 33(55)
2.1 Introduction To Fluid Dynamics
34(2)
2.2 Conservation Of Mass
36(4)
2.3 Conservation Of Linear Momentum
40(6)
2.4 Applications To Constant-Property Flows
46(9)
2.5 Reynolds Number And Mach Number As Similarity Parameters
55(8)
2.6 Concept Of The Boundary Layer
63(2)
2.7 Conservation Of Energy
65(1)
2.8 First Law Of Thermodynamics
66(2)
2.9 Derivation Of The Energy Equation
68(8)
2.10 Summary
76(1)
Problems
76(11)
References
87(1)
Chapter 3 Dynamics Of An Incompressible, Inviscid Flow Field 88(78)
3.1 Inviscid Flows
89(1)
3.2 Bernoulli's Equation
90(3)
3.3 Use Of Bernoulli's Equation To Determine Airspeed
93(3)
3.4 The Pressure Coefficient
96(3)
3.5 Circulation
99(3)
3.6 Irrotational Flow
102(1)
3.7 Kelvin's Theorem
103(1)
3.8 Incompressible, Irrotational Flow And The Velocity Potential
104(3)
3.9 Stream Function In A Two-Dimensional, Incompressible Flow
107(2)
3.10 Relation Between Streamlines And Equipotential Lines
109(3)
3.11 Superposition Of Flows
112(1)
3.12 Elementary Flows
113(13)
3.13 Adding Elementary Flows To Describe Flow Around A Cylinder
126(8)
3.14 Lift And Drag Coefficients As Dimensionless Flow-Field Parameters
134(5)
3.15 Flow Around A Cylinder With Circulation
139(5)
3.16 Source Density Distribution On The Body Surface
144(5)
3.17 Incompressible, Axisymmetric Flow
149(3)
3.18 Summary
152(1)
Problems
152(13)
References
165(1)
Chapter 4 Viscous Boundary Layers 166(60)
4.1 Equations Governing The Boundary Layer For A Steady, Two-Dimensional, Incompressible Flow
167(3)
4.2 Boundary Conditions
170(1)
4.3 Incompressible, Laminar Boundary Layer
171(18)
4.4 Boundary-Layer Transition
189(4)
4.5 Incompressible, Turbulent Boundary Layer
193(9)
4.6 Eddy Viscosity And Mixing Length Concepts
202(2)
4.7 Integral Equations For A Flat-Plate Boundary Layer
204(11)
4.8 Thermal Boundary Layer For Constant-Property Flows
215(6)
4.9 Summary
221(1)
Problems
221(4)
References
225(1)
Chapter 5 Characteristic Parameters For Airfoil And Wing Aerodynamics 226(68)
5.1 Characterization Of Aerodynamic Forces And Moments
227(4)
5.2 Airfoil Geometry Parameters
231(5)
5.3 Wing-Geometry Parameters
236(8)
5.4 Aerodynamic Force And Moment Coefficients
244(29)
5.5 Wings Of Finite Span
273(15)
Problems
288(4)
References
292(2)
Chapter 6 Incompressible Flows Around Airfoils Of Infinite Span 294(47)
6.1 General Comments
295(1)
6.2 Circulation And The Generation Of Lift
296(2)
6.3 General Thin-Airfoil Theory
298(3)
6.4 Thin, Flat-Plate Airfoil (Symmetric Airfoil)
301(5)
6.5 Thin, Cambered Airfoil
306(11)
6.6 Laminar-Flow Airfoils
317(4)
6.7 High-Lift Airfoil Sections
321(6)
6.8 Multielement Airfoil Sections For Generating High Lift
327(7)
6.9 High-Lift Military Airfoils
334(3)
Problems
337(2)
References
339(2)
Chapter 7 Incompressible Flow About Wings Of Finite Span 341(90)
7.1 General Comments
342(3)
7.2 Vortex System
345(1)
7.3 Lifting-Line Theory For Unswept Wings
346(29)
7.4 Panel Methods
375(4)
7.5 Vortex Lattice Method
379(22)
7.6 Factors Affecting Drag Due-To-Lift At Subsonic Speeds
401(3)
7.7 Delta Wings
404(10)
7.8 Leading-Edge Extensions
414(4)
7.9 Asymmetric Loads On The Fuselage At High Angles Of Attack
418(4)
7.10 Flow Fields For Aircraft At High Angles Of Attack
422(2)
7.11 Unmanned Air Vehicle Wings
424(2)
7.12 Summary
426(1)
Problems
426(2)
References
428(3)
Chapter 8 Dynamics Of A Compressible Flow Field 431(74)
8.1 Thermodynamic Concepts
432(9)
8.2 Adiabatic Flow In A Variable-Area Streamtube
441(4)
8.3 Isentropic Flow In A Variable-Area Streamtube
445(6)
8.4 Converging-Diverging Nozzles
451(3)
8.5 Characteristic Equations And Prandtl-Meyer Flows
454(8)
8.6 Shock Waves
462(11)
8.7 Viscous Boundary Layer
473(7)
8.8 Shock-Wave/Boundary-Layer Interactions
480(2)
8.9 Shock/Shock Interactions
482(4)
8.10 The Role Of Experiments For Generating Information Defining The Flow Field
486(8)
8.11 Comments About The Scaling/correction Process(Es) For Relatively Clean Cruise Configurations
494(1)
8.12 Summary
495(1)
Problems
495(7)
References
502(3)
Chapter 9 Compressible, Subsonic Flows And Transonic Flows 505(46)
9.1 Compressible, Subsonic Flow
506(11)
9.2 Transonic Flow Past Unswept Airfoils
517(9)
9.3 Wave Drag Reduction By Design
526(1)
9.4 Swept Wings At Transonic Speeds
527(16)
9.5 Transonic Aircraft
543(5)
9.6 Summary
548(1)
Problems
548(1)
References
548(3)
Chapter 10 Two-Dimensional, Supersonic Flows Around Thin Airfoils 551(26)
10.1 Linear Theory
553(8)
10.2 Second-Order Theory (Busemann's Theory)
561(5)
10.3 Shock-Expansion Technique
566(6)
10.4 Summary
572(1)
Problems
572(3)
References
575(2)
Chapter 11 Supersonic Flows Over Wings And Airplane Configurations 577(72)
11.1 General Remarks About Lift And Drag
579(2)
11.2 General Remarks About Supersonic Wings
581(2)
11.3 Governing Equation And Boundary Conditions
583(1)
11.4 Consequences Of Linearity
584(1)
11.5 Solution Methods
585(1)
11.6 Conical-Flow Method
585(13)
11.7 Singularity-Distribution Method
598(27)
11.8 Design Considerations For Supersonic Aircraft
625(2)
11.9 Some Comments About The Design Of The SST And Of The HSCT
627(7)
11.10 Slender Body Theory
634(2)
11.11 Base Drag
636(3)
11.12 Aerodynamic Interaction
639(3)
11.13 Aerodynamic Analysis For Complete Configurations In A Supersonic Free Stream
642(1)
11.14 Summary
643(1)
Problems
644(2)
References
646(3)
Chapter 12 Hypersonic Flows 649(62)
12.1 The Five Distinguishing Characteristics
652(5)
12.2 Newtonian Flow Model
657(3)
12.3 Stagnation Region Flow-Field Properties
660(5)
12.4 Modified Newtonian Flow
665(17)
12.5 High L/D Hypersonic Configurations-waveriders
682(9)
12.6 Aerodynamic Heating
691(6)
12.7 A Hypersonic Cruiser For The Twenty-First Century?
697(3)
12.8 Importance Of Interrelating CFD, Ground-Test Data, And Flight-Test Data
700(2)
12.9 Boundary-Layer-Transition Methodology
702(4)
12.10 Summary
706(1)
Problems
706(2)
References
708(3)
Chapter 13 Aerodynamic Design Considerations 711(64)
13.1 High-Lift Configurations
712(13)
13.2 Circulation Control Wing
725(2)
13.3 Design Considerations For Tactical Military Aircraft
727(4)
13.4 Drag Reduction
731(11)
13.5 Development Of An Airframe Modification To Improve The Mission Effectiveness Of An Existing Airplane
742(16)
13.6 Considerations For Wing/canard, Wing/Tail, And Tailless Configurations
758(5)
13.7 Comments On The F-15 Design
763(1)
13.8 The Design Of The F-22
764(3)
13.9 The Design Of The F-35
767(3)
13.10 Summary
770(1)
Problems
770(2)
References
772(3)
Chapter 14 Tools For Defining The Aerodynamic Environment 775(17)
14.1 Computational Tools
777(6)
14.2 Establishing The Credibility Of CFD Simulations
783(2)
14.3 Ground-Based Test Programs
785(3)
14.4 Flight-Test Programs
788(1)
14.5 Integration Of Experimental And Computational Tools: The Aerodynamic Design Philosophy
789(1)
14.6 Summary
790(1)
References
790(2)
Appendix A The Equations Of Motion Written In Conservation Form 792(6)
Appendix B A Collection Of Often Used Tables 798(8)
Answers To Selected Problems 806(5)
Credits 811(4)
Index 815(12)
Conversion Factors 827
John J. Bertin, deceased, was Professor Emeritus of Aeronautics at the US Air Force Academy, formerly holding positions at NASA, The University of Texas at Austin, and Sandia National Laboratories. Russell M. Cummings is Professor of Aeronautics at the US Air Force Academy. He is a Fellow of the American Institute of Aeronautics and the Royal Aeronautical Society, and the lead author of Applied Computational Aerodynamics (Cambridge University Press, 2015).
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