| Chapter I. Concepts from thermodynamics |
|   | 1.1 Introduction |
|   | 1.2 Thermodynamic Systems |
|   | 1.3 Variables of state |
|   | 1.4 The first principal law |
|   | 1.5 Irreversible and reversible processes |
|   | 1.6 Perfect Gases |
|   | 1.7 The first Law applied to reversible processes. Specific Heats |
|   | 1.8 The first Law applied to irreversible processes |
|   | 1.9 The concept of Entropy. The Second Law |
|   | 1.10 The Canonical equation of state. Free energy and free enthalpy |
|   | 1.11 Reciprocity relations |
|   | 1.12 Entropy and transport processes |
|   | 1.13 Equilibrium conditions |
|   | 1.14 Mixtures of perfect gases |
|   | 1.15 The law of mass action |
|   | 1.16 Dissociation |
|   | 1.17 Condensation |
|   | 1.18 Real Gases in Gasdynamics |
| Chapter 2. One-dimensional gasdynamics |
|   | 2.1 Introduction |
|   | 2.2 The continuity equation |
|   | 2.3 The energy equation |
|   | 2.4 Reservoir conditions |
|   | 2.5 Euler's equation |
|   | 2.6 The momentum equation |
|   | 2.7 Isentropic conditions |
|   | 2.8 Speed of sound; mach number |
|   | 2.9 The Area-velocity relation |
|   | 2.10 Results from the energy equation |
|   | 2.11 Bernoulli equation; dynamic pressure |
|   | 2.12 Flow at constant Area |
|   | 2.13 The normal shock relations for a perfect Gas |
| Chapter 3. One-dimensional Wave motion |
|   | 3.1 Introduction |
|   | 3.2 The propagating shock wave |
|   | 3.3 One-dimensional isentropic equations |
|   | 3.4 The Acoustic equations |
|   | 3.5 Propagation of Acoustic Waves |
|   | 3.6 The speed of sound |
|   | 3.7 Pressure and Particle Velocity in a sound wave |
|   | 3.8 "Linearized" shock tube |
|   | 3.9 Isentropic Waves of Finite Amplitude |
|   | 3.10 Propagation of Finite Waves |
|   | 3.11 Centered Expansion Wave |
|   | 3.12 The Shock Tube |
| Chapter 4. Waves in supersonic flow |
|   | 4.1 Introduction |
|   | 4.2 Oblique shock |
|   | 4.3 Relation between beta and theta |
|   | 4.4 Supersonic flow over a wedge |
|   | 4.5 Mach lines |
|   | 4.6 Piston analogy |
|   | 4.7 Weak oblique shocks |
|   | 4.8 Supersonic compression by turning |
|   | 4.9 Supersonic expansion by turning |
|   | 4.10 The Prandtl-Meyer function |
|   | 4.11 Simple and nonsimple regions |
|   | 4.12 Reflection and intersection of oblique shocks |
|   | 4.13 Intersection of Shocks of the same family |
|   | 4.14 Detached shocks |
|   | 4.15 Mach reflection |
|   | 4.16 Shock-expansion theory |
|   | 4.17 Thin airfoil theory |
|   | 4.18 Flat lifting wings |
|   | 4.19 Drag reduction |
|   | 4.20 The Hodograph Plane |
|   | 4.21 Cone in supersonic flow |
| Chapter 5. Flow in ducts and wind tunnels |
|   | 5.1 Introduction |
|   | 5.2 Flow in Channel of Varying Area |
|   | 5.3 Area Relations |
|   | 5.4 Nozzle Flow |
|   | 5.5 Normal Shock recovery |
|   | 5.6 Effects of second throat |
|   | 5.7 Actual performance of wind tunnel diffusers |
|   | 5.8 Wind tunnel pressure ratio |
|   | 5.9 Supersonic wind tunnels |
|   | 5.10 Wind tunnel Characteristics |
|   | 5.11 Compressor Matching |
|   | 5.12 Other wind tunnels and testing methods |
| Chapter 6. Methods of measurement |
|   | 6.1 Introduction |
|   | 6.2 Static pressure |
|   | 6.3 Total pressure |
|   | 6.4 Mach number from pressure measurements |
|   | 6.5 Wedge and cone measurements |
|   | 6.6 Velocity |
|   | 6.7 Temperature and Heat transfer measurements |
|   | 6.8 Density measurements |
|   | 6.9 Index of refraction |
|   | 6.10 Schlieren system |
|   | 6.11 The knife edge |
|   | 6.12 Some practical considerations |
|   | 6.13 The shadow method |
|   | 6.14 Interference method |
|   | 6.15 Mach-Zehnder Interferometer |
|   | 6.16 Interferometer Techniques |
|   | 6.17 X-Ray absorption and other me |
|   | 6.18 Direct measurement of skin friction |
|   | 6.19 Hot-wire probe |
|   | 6.20 Shock tube instrumentation |
| Chapter 7. The equations of frictionless flow |
|   | 7.1 Introduction |
|   | 7.2 Notation |
|   | 7.3 The equation of continuity |
|   | 7.4 The momentum equation |
|   | 7.5 The energy equation |
|   | 7.6 The eulerian derivative |
|   | 7.7 Splitting the energy equation |
|   | 7.8 The total enthalpy |
|   | 7.9 Natural coordinates. Crocco's theorem |
|   | 7.10 Relation of vorticity to circulation and rotation |
|   | 7.11 The velocity potential |
|   | 7.12 Irrotational flow |
|   | 7.13 Remarks on the equations of motion |
| Chapter 8. Small-perturbation theory |
|   | 8.1 Introduction |
|   | 8.2 Derivation of the Perturbation equations |
|   | 8.3 Pressure coefficient |
|   | 8.4 Boundary conditions |
|   | 8.5 Two-dimensional flow past a wave-shaped wall |
|   | 8.6 Wavy wall in supersonic flow |
|   | 8.7 Supersonic thin airfoil theory |
|   | 8.8 Planar flows |
| Chapter 9. Bodies of revolution. Slender body theory |
|   | 9.1 Introduction |
|   | 9.2 Cylindrical coordinates |
|   | 9.3 Boundary conditions |
|   | 9.4 Pressure coefficient |
|   | 9.5 Axially symmetric flow |
|   | 9.6 Subsonic flow |
|   | 9.7 Supersonic flow |
|   | 9.8 Velocities in the Supersonic field |
|   | 9.9 Solution for a Cone |
|   | 9.10 Other meridian shapes |
|   | 9.11 Solution for Slender Cone |
|   | 9.12 Slender Body Drag |
|   | 9.13 Yawed body of revolution in supersonic flow |
|   | 9.14 Cross-flow boundary conditions |
|   | 9.15 Cross-flow solutions |
|   | 9.16 Cross flow for slender bodies of revolution |
|   | 9.17 Lift of slender bodies of revolution |
|   | 9.18 Slender body theory |
|   | 9.19 Rayleigh's formula |
| Chapter 10. The similarity rules of high-speed flow |
|   | 10.1 Introduction |
|   | 10.2 Two-dimensional linearized flow. Prandtl-Glauert and Göthert |
|   | 10.3 Two-dimensional transonic flow. von Kármán's rules |
|   | 10.4 Linearized axially symmetric flow |
|   | 10.5 Planar flow |
|   | 10.6 Summary and application of the similarity laws |
|   | 10.7 High mach numbers. Hypersonic similarity |
| Chapter 11. Transonic flow |
|   | 11.1 Introduction |
|   | 11.2 Definition of the transonic range |
|   | 11.3 Transonic flow past wedge sections |
|   | 11.4 Transonic flow past a cone |
|   | 11.5 Transonic flow past smooth two-dimensional shapes. The question of shock-free flow |
|   | 11.6 The hodograph transformation of the equations |
| Chapter 12. The method of characteristics |
|   | 12.1 Introduction |
|   | 12.2 Hyperbolic equations |
|   | 12.3 The compatibility relation |
|   | 12.4 The computation method |
|   | 12.5 Interior and boundary points |
|   | 12.6 Axially symmetric flow |
|   | 12.7 Nonisentropic flow |
|   | 12.8 Theorems about Plane flow |
|   | 12.9 Computation with weak, finite waves |
|   | 12.10 Interaction of waves |
|   | 12.11 Design of supersonic nozzles |
|   12.12 Comparison of characteristics and waves |
| Chapter 13. Effects of viscosity and conductivity |
|   | 13.1 Introduction |
|   | 13.2 Couette flow |
|   | 13.3 Recovery temperature |
|   | 13.4 Velocity distribution in couette flow |
|   | 13.5 Rayleigh's problem. The diffusion of vorticity |
|   | 13.6 The boundary-layer concept |
|   | 13.7 Prandtl's equations for a flat plate |
|   | 13.8 Characteristic results from the boundary-layer equation |
|   | 13.9 The displacement effect of the boundary layer. Momentum and energy integrals |
|   | 13.10 Change of variables |
|   | 13.11 Boundary layers of profiles other than a flat plate |
|   | 13.12 Flow through a shock wave |
|   | 13.13 The Navier-Stokes equations |
|   | 13.14 The turbulent boundary layer |
|   | 13.15 Boundary-layer effects on the external flow field |
|   | 13.16 Shock-wave boundary-layer interaction |
|   | 13.17 Turbulence |
|   | 13.18 Couette flow of a dissociating gas |
| Chapter 14. Concepts from gaskinetics |
|   | 14.1 Introdu |
|   | 14.2 Probability conc |
|   | 14.9 Shear viscosity and heat conduction |
|   | 14.10 Couette flow of a highly rarefied gas |
|   | 14.11 The concepts of slip and accommodation |
|   | 14.12 Relaxation effects of the internal degrees of freedom |
|   | 14.13 The limit of continuum theory |
|   | Exercises; Selected references; Tables |
| 1. Critical Data and characteristic temperatures for several gases |
| 2. Flow parameters versus M for Subsonic flow |
| 3. Flow parameters versus M for supersonic flow |
| 4. Parameters for shock flow |
| 5. Mach number and Mach angle versus Prandtl-Meyer function |
|   Charts |
| 1, 2 Oblique shock chart |
|   Appendix, Index |