| Preface to the Second Edition | 5 |
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| Acknowledgements | 7 |
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| Preface to the First Edition | 8 |
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| Acknowledgements | 10 |
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| Table of Contents | 11 |
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| Introduction | 16 |
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| 1.1 Classes of Hypersonic Vehicles and TheirAerothermodynamic Peculiarities | 16 |
| 1.2 RV-Type and CAV-Type Flight Vehicles asReference Vehicles | 20 |
| 1.3 The Tasks of Aerothermodynamics | 26 |
| 1.4 The Thermal State of the Surface and ThermalSurface Effects | 28 |
| 1.5 Unsteady Flight and Steady Aerothermodynamics? | 32 |
| 1.6 Scope and Content of the Book | 33 |
| References | 35 |
| The Flight Environment | 37 |
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| 2.1 The Earth Atmosphere | 37 |
| 2.2 Atmospheric Properties and Models | 42 |
| 2.3 Flow Regimes | 44 |
| 2.4 Problems | 48 |
| References | 48 |
| Thermal Radiation Cooling of ExternalVehicle Surfaces | 50 |
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| 3.1 Definitions | 50 |
| 3.2 The Radiation-Adiabatic Vehicle Surface | 54 |
| 3.3 Case Study: The Thermal State of the Surface ofthe Blunt Delta Wing | 76 |
| 3.4 Summary of the Results of the Chapter in Viewof Flight-Vehicle Design | 85 |
| 3.5 Problems | 86 |
| References | 87 |
| Transport of Momentum, Energy, and Mass | 90 |
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| 4.1 Transport Phenomena | 91 |
| 4.2 Transport Properties | 95 |
| 4.3 Equations of Motion, Initial Conditions, BoundaryConditions, and Similarity Parameters | 103 |
| 4.4 Remarks on Similarity Parameters | 119 |
| 4.5 Problems | 120 |
| References | 120 |
| Real-Gas Aerothermodynamic Phenomena | 123 |
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| 5.1 Van der Waals Effects | 124 |
| 5.2 High-Temperature Real-Gas Effects | 126 |
| 5.3 Dissociation and Recombination | 130 |
| 5.4 Thermal and Chemical Rate Processes | 131 |
| 5.5 Rate Effects, Two Examples | 135 |
| 5.6 Surface Catalytic Recombination | 143 |
| 5.7 A Few Remarks on Simulation Issues | 150 |
| 5.8 Computation Models | 151 |
| 5.9 Problems | 152 |
| References | 153 |
| Inviscid Aerothermodynamic Phenomena | 156 |
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| 6.1 Hypersonic Flight Vehicles and Shock Waves | 157 |
| 6.2 One-Dimensional Shock-Free Flow | 163 |
| 6.3 Shock Waves | 167 |
| 6.4 Blunt-Body Flow | 187 |
| 6.5 Supersonic Turning: Prandtl-Meyer Expansion andIsentropic Compression | 199 |
| 6.6 The Change of the Unit Reynolds Number acrossShock Waves | 203 |
| 6.7 Newton Flow | 207 |
| 6.8 The Mach-Number Independence Principle ofOswatitsch | 215 |
| 6.9 Problems | 221 |
| References | 222 |
| Attached High-Speed Viscous Flow | 225 |
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| 7.1 Attached Viscous Flow | 226 |
| 7.2 Basic Properties of Attached Viscous Flow | 250 |
| 7.3 Case Study: Wall Temperature and Skin Frictionat the S¨ANGER Forebody | 279 |
| 7.4 Problems | 285 |
| References | 286 |
| Laminar-Turbulent Transition and Turbulencein High-Speed Viscous Flow | 289 |
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| 8.1 Laminar-Turbulent Transition as Hypersonic FlowPhenomenon | 292 |
| 8.2 Real Flight-Vehicle Effects | 305 |
| 8.3 Receptivity Issues | 317 |
| 8.4 Prediction of Stability/Instability and Transitionin High-Speed Flows | 323 |
| 8.5 Turbulence Modeling for High-Speed Flows | 330 |
| References | 333 |
| Strong Interaction Phenomena | 342 |
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| 9.1 Flow Separation | 343 |
| 9.2 Shock/Boundary-Layer Interaction Phenomena | 350 |
| 9.3 Hypersonic Viscous Interaction | 365 |
| 9.4 Low-Density Effects | 376 |
| 9.5 Problems | 383 |
| References | 383 |
| Viscous Thermal Surface Effects: Examples | 388 |
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| 10.1 Introduction | 388 |
| 10.2 Qualitative Considerations | 389 |
| 10.3 Examples in Foregoing Chapters | 391 |
| 10.4 Boundary-Layer Thickness at a Heated Wall | 392 |
| 10.5 Displacement Thickness at a Highly Cooled Wall | 394 |
| 10.6 Cone-Flow Experiment: Amplification of theSecond Instability Mode by Cooling | 395 |
| 10.7 Reduction of the Turbulent Skin Friction withSide Effects | 397 |
| 10.8 Flat Plate/Ramp: Length of the Separation Zone | 399 |
| 10.9 Generic Scramjet Inlet: The Shock-on-LipSituation | 403 |
| 10.10 Problems | 405 |
| References | 406 |
| Solution Guide and Solutions of the Problems | 407 |
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| Appendix A | 420 |
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| Appendix B | 424 |
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| Appendix C | 429 |
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| Permissions | 436 |
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| Name Index | 437 |
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| Subject Index | 443 |