: Ernst Heinrich Hirschel
: Basics of Aerothermodynamics
: Springer-Verlag
: 9783319143736
: 2
: CHF 151.90
:
: Luft- und Raumfahrttechnik
: English
: 446
: Wasserzeichen/DRM
: PC/MAC/eReader/Tablet
: PDF

This successful book gives an introduction to the basics of aerothermodynamics, as applied in particular to winged re-entry vehicles and airbreathing hypersonic cruise and acceleration vehicles. The book gives a review of the issues of transport of momentum, energy and mass, real-gas effects as well as inviscid and viscous flow phenomena. In this second, revised edition the chapters with the classical topics of aerothermodynamics more or less were left untouched. The access to some single topics of practical interest was improved. Auxiliary chapters were put into an appendix. The recent successful flights of the X-43A and the X-51A indicate that the dawn of sustained airbreathing hypersonic flight now has arrived. This proves that the original approach of the book to put emphasis on viscous effects and the aerothermodynamics of radiation-cooled vehicle surfaces was timely. This second, revised edition even more accentuates these topics. A new, additional chapter treats examples of viscous thermal surface effects. Partly only very recently obtained experimental and numerical results show the complexity of such phenomena (dependence of boundary-layer stability, skin friction, boundary-layer thicknesses, and separation on the thermal state of the surface) and their importance for airbreathing hypersonic flight vehicles, but also for any other kind of hypersonic vehicle.

Preface to the Second Edition5
Acknowledgements7
Preface to the First Edition8
Acknowledgements10
Table of Contents11
Introduction16
1.1 Classes of Hypersonic Vehicles and TheirAerothermodynamic Peculiarities16
1.2 RV-Type and CAV-Type Flight Vehicles asReference Vehicles20
1.3 The Tasks of Aerothermodynamics26
1.4 The Thermal State of the Surface and ThermalSurface Effects28
1.5 Unsteady Flight and Steady Aerothermodynamics?32
1.6 Scope and Content of the Book33
References35
The Flight Environment37
2.1 The Earth Atmosphere37
2.2 Atmospheric Properties and Models42
2.3 Flow Regimes44
2.4 Problems48
References48
Thermal Radiation Cooling of ExternalVehicle Surfaces50
3.1 Definitions50
3.2 The Radiation-Adiabatic Vehicle Surface54
3.3 Case Study: The Thermal State of the Surface ofthe Blunt Delta Wing76
3.4 Summary of the Results of the Chapter in Viewof Flight-Vehicle Design85
3.5 Problems86
References87
Transport of Momentum, Energy, and Mass90
4.1 Transport Phenomena91
4.2 Transport Properties95
4.3 Equations of Motion, Initial Conditions, BoundaryConditions, and Similarity Parameters103
4.4 Remarks on Similarity Parameters119
4.5 Problems120
References120
Real-Gas Aerothermodynamic Phenomena123
5.1 Van der Waals Effects124
5.2 High-Temperature Real-Gas Effects126
5.3 Dissociation and Recombination130
5.4 Thermal and Chemical Rate Processes131
5.5 Rate Effects, Two Examples135
5.6 Surface Catalytic Recombination143
5.7 A Few Remarks on Simulation Issues150
5.8 Computation Models151
5.9 Problems152
References153
Inviscid Aerothermodynamic Phenomena156
6.1 Hypersonic Flight Vehicles and Shock Waves157
6.2 One-Dimensional Shock-Free Flow163
6.3 Shock Waves167
6.4 Blunt-Body Flow187
6.5 Supersonic Turning: Prandtl-Meyer Expansion andIsentropic Compression199
6.6 The Change of the Unit Reynolds Number acrossShock Waves203
6.7 Newton Flow207
6.8 The Mach-Number Independence Principle ofOswatitsch215
6.9 Problems221
References222
Attached High-Speed Viscous Flow225
7.1 Attached Viscous Flow226
7.2 Basic Properties of Attached Viscous Flow250
7.3 Case Study: Wall Temperature and Skin Frictionat the S¨ANGER Forebody279
7.4 Problems285
References286
Laminar-Turbulent Transition and Turbulencein High-Speed Viscous Flow289
8.1 Laminar-Turbulent Transition as Hypersonic FlowPhenomenon292
8.2 Real Flight-Vehicle Effects305
8.3 Receptivity Issues317
8.4 Prediction of Stability/Instability and Transitionin High-Speed Flows323
8.5 Turbulence Modeling for High-Speed Flows330
References333
Strong Interaction Phenomena342
9.1 Flow Separation343
9.2 Shock/Boundary-Layer Interaction Phenomena350
9.3 Hypersonic Viscous Interaction365
9.4 Low-Density Effects376
9.5 Problems383
References383
Viscous Thermal Surface Effects: Examples388
10.1 Introduction388
10.2 Qualitative Considerations389
10.3 Examples in Foregoing Chapters391
10.4 Boundary-Layer Thickness at a Heated Wall392
10.5 Displacement Thickness at a Highly Cooled Wall394
10.6 Cone-Flow Experiment: Amplification of theSecond Instability Mode by Cooling395
10.7 Reduction of the Turbulent Skin Friction withSide Effects397
10.8 Flat Plate/Ramp: Length of the Separation Zone399
10.9 Generic Scramjet Inlet: The Shock-on-LipSituation403
10.10 Problems405
References406
Solution Guide and Solutions of the Problems407
Appendix A420
Appendix B424
Appendix C429
Permissions436
Name Index437
Subject Index443