
Automotive Aerodynamics
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"This is where the book by Katz excels and the fundamental fluid principles are extensively covered under a vehicle aerodynamics title"...."Katz's book will make a prime choice textbook for an undergraduate Automotive Engineering course, as fluid related modules in various academic years can cover the topics presented in various chapters of the book" Remus Cîrstea, Course Director MSc Automotive Engineering, Lecturer in Fluid Dynamics, Coventry University on behalf of The Aeronautical Jornal, Oct 2017Weitere Details
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Joseph Katz, San Diego State University, USA
Inhalt
Series Preface xii
Preface xiv
1 Introduction and Basic Principles 1
1.1 Introduction 1
1.2 Aerodynamics as a Subset of Fluid Dynamics 2
1.3 Dimensions and Units 3
1.4 Automobile/Vehicle Aerodynamics 5
1.5 General Features of Fluid Flow 9
1.5.1 Continuum 10
1.5.2 Laminar and Turbulent Flow 11
1.5.3 Attached and Separated Flow 12
1.6 Properties of Fluids 13
1.6.1 Density 13
1.6.2 Pressure 14
1.6.3 Temperature 14
1.6.4 Viscosity 16
1.6.5 Specific Heat 19
1.6.6 Heat Transfer Coefficient, k 19
1.6.7 Modulus of Elasticity, E 20
1.6.8 Vapor Pressure 22
1.7 Advanced Topics: Fluid Properties and the Kinetic Theory of Gases 23
1.8 Summary and Concluding Remarks 26
Reference 27
Problems 27
2 The Fluid Dynamic Equations 35
2.1 Introduction 35
2.2 Description of Fluid Motion 36
2.3 Choice of Coordinate System 38
2.4 Pathlines, Streak Lines, and Streamlines 39
2.5 Forces in a Fluid 40
2.6 Integral Form of the Fluid Dynamic Equations 43
2.7 Differential Form of the Fluid Dynamic Equations 50
2.8 The Material Derivative 57
2.9 Alternate Derivation of the Fluid Dynamic Equations 59
2.10 Example for an Analytic Solution: Two-Dimensional, Inviscid Incompressible, Vortex Flow 62
2.10.1 Velocity Induced by a Straight Vortex Segment 65
2.10.2 Angular Velocity, Vorticity, and Circulation 66
2.11 Summary and Concluding Remarks 69
References 72
Problems 72
3 One-Dimensional (Frictionless) Flow 81
3.1 Introduction 81
3.2 The Bernoulli Equation 82
3.3 Summary of One-Dimensional Tools 84
3.4 Applications of the One-Dimensional Friction-Free Flow Model 85
3.4.1 Free Jets 85
3.4.2 Examples for Using the Bernoulli Equation 89
3.4.3 Simple Models for Time-Dependent Changes in a Control Volume 93
3.5 Flow Measurements (Based on Bernoulli's Equation) 96
3.5.1 The Pitot Tube 96
3.5.2 The Venturi Tube 98
3.5.3 The Orifice 100
3.5.4 Nozzles and Injectors 101
3.6 Summary and Conclusions 102
3.6.1 Concluding Remarks 103
Problems 104
4 Dimensional Analysis, High Reynolds Number Flows, and Definition of Aerodynamics 122
4.1 Introduction 122
4.2 Dimensional Analysis of the Fluid Dynamic Equations 123
4.3 The Process of Simplifying the Governing Equations 126
4.4 Similarity of Flows 127
4.5 High Reynolds Number Flow and Aerodynamics 129
4.6 High Reynolds Number Flows and Turbulence 133
4.7 Summary and Conclusions 136
References 136
Problems 136
5 The Laminar Boundary Layer 141
5.1 Introduction 141
5.2 Two-Dimensional Laminar Boundary Layer Model - The Integral Approach 143
5.3 Solutions using the von Kármán Integral Equation 147
5.4 Summary and Practical Conclusions 156
5.5 Effect of Pressure Gradient 161
5.6 Advanced Topics: The Two-Dimensional Laminar Boundary Layer Equations 164
5.6.1 Summary of the Exact Blasius Solution for the Laminar Boundary Layer 167
5.7 Concluding Remarks 169
References 170
Problems 170
6 High Reynolds Number Incompressible Flow Over Bodies: Automobile Aerodynamics 176
6.1 Introduction 176
6.2 The Inviscid Irrotational Flow (and Some Math) 178
6.3 Advanced Topics: A More Detailed Evaluation of the Bernoulli Equation 181
6.4 The Potential Flow Model 183
6.4.1 Methods for Solving the Potential Flow Equations 183
6.4.2 The Principle of Superposition 184
6.5 Two-Dimensional Elementary Solutions 184
6.5.1 Polynomial Solutions 185
6.5.2 Two-Dimensional Source (or Sink) 187
6.5.3 Two-Dimensional Doublet 190
6.5.4 Two-Dimensional Vortex 193
6.5.5 Advanced Topics: Solutions Based on Green's Identity 196
6.6 Superposition of a Doublet and a Free-Stream: Flow Over a Cylinder 199
6.7 Fluid Mechanic Drag 204
6.7.1 The Drag of Simple Shapes 205
6.7.2 The Drag of More Complex Shapes 210
6.8 Periodic Vortex Shedding 215
6.9 The Case for Lift 218
6.9.1 A Cylinder with Circulation in a Free Stream 218
6.9.2 Two-Dimensional Flat Plate at a Small Angle of Attack (in a Free Stream) 222
6.9.3 Note About the Center of Pressure 224
6.10 Lifting Surfaces: Wings and Airfoils 225
6.10.1 The Two-Dimensional Airfoil 226
6.10.2 An Airfoil's Lift 228
6.10.3 An Airfoil's Drag 229
6.10.4 An Airfoil Stall 231
6.10.5 The Effect of Reynolds Number 232
6.10.6 Three-Dimensional Wings 233
6.11 Summary of High Reynolds Number Aerodynamics 248
6.12 Concluding Remarks 249
References 249
Problems 250
7 Automotive Aerodynamics: Examples 262
7.1 Introduction 262
7.2 Generic Trends (For Most Vehicles) 263
7.2.1 Ground Effect 264
7.2.2 Generic Automobile Shapes and Vortex Flows 265
7.3 Downforce and Vehicle Performance 269
7.4 How to Generate Downforce 274
7.5 Tools used for Aerodynamic Evaluations 274
7.5.1 Example for Aero Data Collection: Wind Tunnels 276
7.5.2 Wind Tunnel Wall/Floor Interference 279
7.5.3 Simulation of Moving Ground 281
7.5.4 Expected Results of CFD, Road, or Wind Tunnel Tests (and Measurement Techniques) 283
7.6 Variable (Adaptive) Aerodynamic Devices 286
7.7 Vehicle Examples 291
7.7.1 Passenger Cars 292
7.7.2 Pickup Trucks 298
7.7.3 Motorcycles 299
7.7.4 Competition Cars (Enclosed Wheel) 302
7.7.5 Open-Wheel Racecars 306
7.8 Concluding Remarks 312
References 314
Problems 314
8 Introduction to Computational Fluid Mechanics (CFD) 316
8.1 Introduction 316
8.2 The Finite-Difference Formulation 317
8.3 Discretization and Grid Generation 320
8.4 The Finite-Difference Equation 321
8.5 The Solution: Convergence and Stability 324
8.6 The Finite-Volume Method 326
8.7 Example: Viscous Flow Over a Cylinder 328
8.8 Potential-Flow Solvers: Panel Methods 331
8.9 Summary 335
References 337
Problems 337
9 Viscous Incompressible Flow: "Exact Solutions" 339
9.1 Introduction 339
9.2 The Viscous Incompressible Flow Equations (Steady State) 340
9.3 Laminar Flow between Two Infinite Parallel Plates: The Couette Flow 340
9.3.1 Flow with a Moving Upper Surface 342
9.3.2 Flow between Two Infinite Parallel Plates: The Results 343
9.3.3 Flow between Two Infinite Parallel Plates - The Poiseuille Flow 347
9.3.4 The Hydrodynamic Bearing (Reynolds Lubrication Theory) 351
9.4 Flow in Circular Pipes (The Hagen-Poiseuille Flow) 359
9.5 Fully Developed Laminar Flow between Two Concentric Circular Pipes 364
9.6 Laminar Flow between Two Concentric, Rotating Circular Cylinders 366
9.7 Flow in Pipes: Darcy's Formula 370
9.8 The Reynolds Dye Experiment, Laminar/Turbulent Flow in Pipes 371
9.9 Additional Losses in Pipe Flow 374
9.10 Summary of 1D Pipe Flow 375
9.10.1 Simple Pump Model 378
9.10.2 Flow in Pipes with Noncircular Cross Sections 379
9.10.3 Examples for One-Dimensional Pipe Flow 381
9.10.4 Network of Pipes 391
9.11 Free Vortex in a Pool 394
9.12 Summary and Concluding Remarks 397
Reference 397
Problems 397
10 Fluid Machinery 411
10.1 Introduction 411
10.2 Work of a Continuous-Flow Machine 415
10.3 The Axial Compressor (The Mean Radius Model) 417
10.3.1 Velocity Triangles 421
10.3.2 Power and Compression Ratio Calculations 424
10.3.3 Radial Variations 429
10.3.4 Pressure Rise Limitations 431
10.3.5 Performance Envelope of Compressors and Pumps 434
10.3.6 Degree of Reaction 441
10.4 The Centrifugal Compressor (or Pump) 446
10.4.1 Torque, Power, and Pressure Rise 447
10.4.2 Impeller Geometry 450
10.4.3 The Diffuser 454
10.4.4 Concluding Remarks: Axial versus Centrifugal Design 457
10.5 Axial Turbines 458
10.5.1 Torque, Power, and Pressure Drop 459
10.5.2 Axial Turbine Geometry and Velocity Triangles 461
10.5.3 Turbine Degree of Reaction 464
10.5.4 Turbochargers (for Internal Combustion Engines) 473
10.5.5 Remarks on Exposed Tip Rotors (Wind Turbines and Propellers) 474
10.6 Concluding Remarks 478
Reference 478
Problems 478
11 Elements of Heat Transfer 485
11.1 Introduction 485
11.2 Elementary Mechanisms of Heat Transfer 486
11.2.1 Conductive Heat Transfer 486
11.2.2 Convective Heat Transfer 489
11.2.3 Radiation Heat Transfer 491
11.3 Heat Conduction 495
11.3.1 Steady One-Dimensional Heat Conduction 497
11.3.2 Combined Heat Transfer 499
11.3.3 Heat Conduction in Cylinders 502
11.3.4 Cooling Fins 506
11.4 Heat Transfer by Convection 515
11.4.1 The Flat Plate Model 516
11.4.2 Formulas for Forced External Heat Convection 520
11.4.3 Formulas for Forced Internal Heat Convection 526
11.4.4 Formulas for Free (Natural) Heat Convection 529
11.5 Heat Exchangers 534
11.6 Concluding Remarks 536
References 539
Problems 539
12 Automobile Aero-Acoustics 544
12.1 Introduction 544
12.2 Sound as a Pressure Wave 546
12.3 Sound Loudness Scale 549
12.4 The Human Ear Perception 552
12.5 The One-Dimensional Linear Wave Equation 553
12.6 Sound Radiation, Transmission, Reflection, Absorption 556
12.6.1 Sound Wave Expansion (Radiation) 556
12.6.2 Reflections, Transmission, Absorption 559
12.6.3 Standing Wave (Resonance), Interference, and Noise Cancellations 560
12.7 Vortex Sound 561
12.8 Example: Sound from a Shear Layer 564
12.9 Buffeting 568
12.10 Experimental Examples for Sound Generation on a Typical Automobile 574
12.11 Sound and Flow Control 576
12.12 Concluding Remarks 577
References 578
Problems 578
Appendix A 581
Appendix B 583
Index 589
1
Introduction and Basic Principles
1.1 Introduction
Wind and water flows played an important role in the evolution of our civilization and provided inspiration in early agriculture, transportation, and even power generation. Ancient ship builders and architects of the land all respected the forces of nature and tried to utilize nature's potential. At the onset of the industrial revolution, as early as the nineteenth century, motorized vehicles appeared and considerations for improved efficiency drove the need to better understand the mechanics of fluid flow. Parallel to that progress the mathematical aspects and the governing equations, called the Navier-Stokes (NS) equations, were established (by the mid-1800s) but analytic solutions didn't follow immediately. The reason of course is the complexity of these nonlinear partial differential equations that have no closed form analytical solution (for an arbitrary case). Consequently, the science of fluid mechanics has focused on simplifying this complex mathematical model and on providing partial solutions for more restricted conditions. This explains why the term fluid mechanics (or dynamics) is used first and not aerodynamics. The reason is that by neglecting lower-order terms in the complex NS equations, simplified solutions can be obtained, which still preserve the dominant physical effects. Aerodynamics therefore is an excellent example for generating useful engineering solutions via "simple" models that were responsible for the huge progress in vehicle development both on the ground and in the air. By focusing on automobile aerodynamics, the problem is simplified even more and we can consider the air as incompressible, contrary to airplanes flying at supersonic speeds.
At this point one must remember the enormous development of computational power in the twenty-first century, which made numerical solution of the fluid mechanic equations a reality. However, in spite of these advances, elements of modeling are still used in those solutions and the understanding of the "classical" but limited models is essential to successfully use those modern tools.
Prior to discussing the airflow over vehicles, some basic definitions, the engineering units to be used, and the properties of air and other fluids must be revisited. After this short introduction, the fluid dynamic equations will be discussed and the field of aerodynamic will be better defined.
1.2 Aerodynamics as a Subset of Fluid Dynamics
The science of fluid mechanics is neither really new nor biblical; although most of the progress in this field was made in the latest century. Therefore, it is appropriate to open this text with a brief history of the discipline with only a very few names mentioned.
As far as we could document history, fluid dynamics and related engineering was always an integral part of human evolution. Ancient civilizations built ships, sails, irrigation systems, or flood management structures, all requiring some basic understanding of fluid flow. Perhaps the best known early scientist in this field is Archimedes of Syracuse (287-212 BC), founder of the field now we call "fluid statics", whose laws on buoyancy and flotation are used to this day.
Major progress in the understanding of fluid mechanics begun with the European Renaissance of the fourteenth to seventeenth centuries. The famous Italian painter sculptor, Leonardo da Vinci (1452-1519) was one of the first to document basic laws such as the conservation of mass. He sketched complex flow fields, suggested viable configuration for airplanes, parachutes, or even helicopters, and introduced the principle of streamlining to reduce drag.
During the next couple of hundred years, sciences gradually developed and then suddenly were accelerated by the rational mathematical approach of Englishman, Sir Isaac Newton (1642-1727) to physics. Apart from his basic laws of mechanics, and particularly the second law connecting acceleration with force, Newton developed the concept for drag and shear in a moving fluid, principles widely used today.
The foundations of fluid mechanics really crystallized in the eighteenth century. One of the more famous scientists, Daniel Bernoulli (1700-1782, Dutch-Swiss) pointed out the relation between velocity and pressure in a moving fluid, the equation of which bears his name in every textbook. However, his friend Leonhard Euler (1707-1783, Swiss born), a real giant in this field is the one actually formulating the Bernoulli equations in the form known today. In addition Euler, using Newton's principles, developed the continuity and momentum equations for fluid flow. These differential equations, the Euler equations are the basis for modern fluid dynamics and perhaps the most significant contribution in the process of understanding fluid flows. Although Euler derived the mathematical formulation, he didn't provide solution to his equations.
Science and experimentation in the field advanced but only in the next century were the governing equations finalized in the form known today. Frenchman, Claude-Louis-Marie-Henri Navier (1785-1836) understood that friction in a flowing fluid must be added to the force balance. He incorporated these terms into the Euler equations, and published the first version of the complete set of equation in 1822. These equations are known today as the Navier-Stokes equations. Communications and information transfer weren't well developed those days. For example, Sir George Gabriel Stokes (1819-1903) lived at the English side of the Channel but didn't communicate directly with Navier. Independently, he also added the viscosity term to the Euler equations, hence the shared glory by naming the equations after both scientists. Stokes can be also considered as the first to solve the equations for the motion of a sphere in a viscous flow, which is now called Stokes flow.
Although the theoretical basis for the governing equation was laid down by now, it was clear that the solution is far from reach and therefore scientists focused on "approximate models" using only portions of the equation, which can be solved. Experimental fluid mechanics also gained momentum, with important discoveries by Englishman Osborne Reynolds (1842-1912) about turbulence and transition from laminar to turbulent flow. This brings us to the twentieth century, when science and technology grew at an explosive rate, particularly, after the first powered flight of the Wright brothers in the US (Dec 1903). Fluid mechanics attracted not only the greatest talent but also investments from governments, as the potential of flying machines was recognized. If we mention one name per century then Ludwig Prandtl (1874-1953) of Gottingen Germany deserves the glory. He made tremendous progress in developing simple models for problems such as boundary layers and airplane wings.
The efforts of Prandtl lead to the initial definition of aerodynamics. His assumptions usually considered low-speed airflow as incompressible, an assumption leading to significant simplifications (as will be explained in Chapter 4). Also, in most cases the effects of viscosity were considered to be confined into a thin boundary layer, so that the viscous flow terms were neglected. These two major simplifications allowed the development of (aerodynamic) models that could be solved analytically and eventually compared well with experimental results!
This trend of solving models and not the complex Navier-Stokes equations continued well into the mid-1990s, until the tremendous growth in computer power finally allowed numerical solution of these equations. Physical modeling is still required but the numerical approach allows the solution of nonlinear partial differential equations, an impossible task from the pure analytical point of view. Nowadays, the flow over complex shapes and the resulting forces can be computed by commercial computer codes but without being exposed to simple models our ability to analyze the results would be incomplete.
1.3 Dimensions and Units
The magnitude (or dimensions) of physical variables is expressed using engineering units. In this text we shall follow the metric system, which was accepted by most professional societies in the mid-1970s. This international system of units (SI) is based on the decimal system and is much easier to use than other (e.g., British) systems of units. For example, the basic length is measured by meters (m) and 1000?m is called a kilometer (km) or 1/100 of a meter is a centimeter. Along the same line 1/1000?m is a millimeter.
Mass is measured in grams, which is the weight of one cubic centimeter of water. One thousand grams are one kilogram (kg) and 1000 kg is one metric ton. Time is still measured the old fashion way, by hours (h) and 1/60th of an hour is a minute (min), while 1/60 of a minute is a second (s).
For the present text velocity is one of the most important variables and its basic measure therefore is m/s. Vehicles speed are usually measured in km/h and clearly 1?km/h = 1000/3600 = 1/3.6 m/s Acceleration is the rate of change of velocity and therefore it is measured by m/s2.
Newton's Second Law defines the units for the force F, when a mass m is accelerated at a rate of a
Therefore, this unit is called Newton (N). Sometimes the unit kilogram-force is used (kgf) since the gravitational pull of 1?kg mass at sea level is...
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