Introduction / 1: |
Three Reference Classes of Hypersonic Vehicles / 1.1: |
Aerothermodynamics and the Definition and Development of Flight Vehicles / 1.2: |
Design Sensitivities and Margins versus Data Uncertainties / 1.2.1: |
Deficits of Aerothermodynamic Simulation Means / 1.2.2: |
Scope and Content of the Book / 1.3: |
References |
Short Introduction to Flight Trajectories for Aerothermodynamicists / 2: |
Flight Trajectories of Winged and Non-Winged Re-Entry Vehicles / 2.1: |
General Aspects / 2.1.1: |
Guidance Objectives, Trajectory Control Variables, and Systems and Operational Constraints / 2.1.2: |
Forces Acting on a Re-Entry Vehicle / 2.1.3: |
The Equilibrium Glide Trajectory / 2.1.4: |
Equilibrium Glide Trajectory: Qualitative Results / 2.1.5: |
Case Study 1: Trajectories of RV-NW's / 2.1.6: |
Case Study 2: Trajectory of a RV-W (X-38) / 2.1.7: |
Flight Trajectories of Cruise and Acceleration Vehicles / 2.2: |
Forces Acting on a Cruise and Acceleration Vehicle / 2.2.1: |
Case Study 3: Trajectory of a CAV (SÄNGER) / 2.2.4: |
General Equations for Planetary Flight / 2.3: |
Problems / 2.4: |
Aerothermodynamic Design Problems of Winged Re-Entry Vehicles / 3: |
Overview of Aerothermodynamic Issues of Winged Re-Entry Vehicles / 3.1: |
Aerothermodynamic Phenomena / 3.1.1: |
Major Simulation Problem: High Mach Number and Total Enthalpy Effects / 3.1.2: |
Particular Trends in RV-W Aerothermodynamics / 3.2: |
Stagnation Pressure / 3.2.1: |
Topology of the Windward Side Velocity Field / 3.2.2: |
Lift Generation / 3.2.3: |
Base Pressure and Drag / 3.2.4: |
Aerodynamic Performance Data of RV-W's / 3.3: |
Space Shuttle Orbiter / 3.3.1: |
HERMES Configuration / 3.3.2: |
HOPE-X Configuration / 3.3.3: |
X-34 Configuration / 3.3.4: |
X-38 Configuration / 3.3.5: |
HOPPER/PHOENIX Configuration / 3.3.6: |
Summary / 3.3.7: |
Vehicle Flyability and Controllability / 3.4: |
General Considerations / 3.4.1: |
Trim and Stability of RV-W's / 3.4.2: |
The Hypersonic Pitching Moment Anomaly of the Space Shuttle Orbiter / 3.5: |
Trim Situation and Possible Causes of the Pitching Moment Anomaly / 3.5.1: |
Pressure Coefficient Distribution at the Windward Side of the Orbiter / 3.5.2: |
The Forward Shift of the Center-of-Pressure / 3.5.3: |
The Hypersonic Pitching Moment Anomaly in View of Oswatitsch's Mach Number Independence Principle / 3.6: |
Wall Pressure Coefficient Distribution / 3.6.1: |
A Simple Analysis of Flight Mach Number and High-Temperature Real Gas Effects / 3.6.3: |
Reconsideration of the Pitching Moment Anomaly and Summary of Results / 3.6.4: |
Concluding Remarks / 3.6.5: |
Aerothermodynamic Design Problems of Winged Airbreathing Vehicles / 3.7: |
Overview of Aerothermodynamic Issues of Cruise and Acceleration Vehicles / 4.1: |
Major Simulation Problem: Viscous Effects / 4.1.1: |
Particular Trends in CAV/ARV Aerothermodynamics / 4.2: |
Topology of the Forebody Windward Side Velocity Field / 4.2.1: |
Aerodynamic Performance / 4.2.3: |
Example: Flight Parameters and Aerodynamic Coefficients of the Reference Concept SÄNGER / 4.3: |
General Configurational Aspects: Highly Coupled Lift and Propulsion System / 4.4: |
Some Vehicle Shape Considerations / 4.4.1: |
Bookkeeping of Aerothermodynamic and Propulsion System Forces / 4.4.2: |
Issues of Aerothermodynamic Airframe/Propulsion Integration / 4.5: |
Forebody Effect / 4.5.1: |
Flat versus Conical Lower Side of Forebody / 4.5.2: |
Principle of Forebody Pre-Compression / 4.5.3: |
Net Thrust Sensitivity on Pre-Compression / 4.5.4: |
Inlet Ramp Flow / 4.5.5: |
Waverider Configurations / 4.6: |
Design Methods / 4.6.1: |
Exemplary Waverider Designs / 4.6.3: |
Influence of Viscous Effects on the Aerodynamic Performance / 4.6.4: |
Off-Design and Low-Speed Behavior / 4.6.5: |
Static Stability Considerations / 4.6.6: |
WaveriderùOperable Vehicle? / 4.6.7: |
Aerothermodynamic Design Problems of Non-Winged Re-Entry Vehicles / 4.7: |
Introduction and Entry Strategies / 5.1: |
Aerobraking / 5.1.1: |
Aerocapturing / 5.1.2: |
Ballistic FlightùBallistic Factor / 5.1.3: |
General Configurational Aspects / 5.2: |
Ballistic Probes / 5.2.1: |
Lifting Capsules / 5.2.2: |
Bicones / 5.2.3: |
Trim Conditions and Static Stability of RV-NW's / 5.3: |
Park's Formula / 5.3.1: |
Performance Data of Lifting Capsules / 5.3.2: |
Controlled Flight and the Role of the Center-of-Gravity / 5.3.3: |
Sensitivity of Aerodynamics against Shape Variations / 5.3.4: |
Parasite Trim / 5.3.5: |
Performance Data of Bicones / 5.3.6: |
Influence of High Temperature, Real Gas Effects on Forces and Moments / 5.3.7: |
Dynamic Stability / 5.4: |
Physics of Dynamic Instability / 5.4.1: |
Equation of Angular Motion / 5.4.2: |
Experimental Methods / 5.4.3: |
Numerical Methods / 5.4.4: |
Typical Experimental Results / 5.4.5: |
Thermal Loads / 5.5: |
OREX Suborbital Flight / 5.5.1: |
ARD Suborbital Flight / 5.5.2: |
APOLLO Low Earth Orbit (LEO) and Lunar Return / 5.5.3: |
VIKING-Type Shape Technology Study / 5.5.4: |
Stabilization, Trim, and Control Devices / 5.6: |
Control Surface Aerothermodynamics, Introduction / 6.1: |
Flap Effectiveness: Influence of the Onset Flow Field / 6.1.1: |
Flap Deflection Modes during Hypersonic Flight / 6.1.2: |
Onset Flow of Aerodynamic Trim and Control Surfaces / 6.2: |
Overall Onset Flow Characteristics / 6.2.1: |
Entropy Layer of the Onset Flow / 6.2.2: |
The Onset Flow Boundary Layer / 6.2.3: |
Asymptotic Consideration of Ramp Flow / 6.3: |
Basic Types of Ramp Flow / 6.3.1: |
Behavior of the Wall Pressure / 6.3.2: |
Behavior of the Thermal State of the Surface / 6.3.3: |
Behavior of the Wall-Shear Stress / 6.3.4: |
Hinge-Line Gap Flow Issues / 6.4: |
Aerothermodynamic Issues of Reaction Control Systems / 6.5: |
Configurational Considerations / 6.6: |
Examples of Stabilization, Trim and Control Devices / 6.6.1: |
Geometrical Considerations / 6.6.2: |
Flap Width versus Flap Length / 6.6.3: |
Volumes of Stabilization and Control Surfaces / 6.6.4: |
Summary of Results / 6.7: |
Simulation Issues / 6.7.2: |
Forces, Moments, Center-of-Pressure, Trim, and Stability in General Formulation / 6.8: |
Moment Equation / 7.1: |
General Formulation of the Center-of-Pressure / 7.2: |
Static Stability Considerations for Bluff Configurations / 7.3: |
Static Stability Considerations for Slender Configurations / 7.4: |
Further Contemplations of Static Stability / 7.5: |
Coordinate Transformations of Force Coefficients / 7.6: |
Multidisciplinary Design Aspects / 7.7: |
Introduction and Short Overview of the Objectives of Multidisciplinary Design Work / 8.1: |
Equations for Fluid-Structure Interaction Domains / 8.2: |
Fluid Dynamics Equations / 8.2.1: |
Structure Dynamics Equations / 8.2.2: |
Heat Transport Equation / 8.2.3: |
Coupling Procedures / 8.3: |
Mechanical Fluid-Structure Interaction Aeroelastic Approach I / 8.3.1: |
Mechanical Fluid-Structure Interaction Aeroelastic Approach II / 8.3.2: |
Thermal-Mechanical Fluid-Structure Interaction / 8.3.3: |
Examples of Coupled Solutions / 8.4: |
Thermal-Fluid-Structure Interaction / 8.4.1: |
Thermal-Mechanical-Fluid-Structure Interaction / 8.4.4: |
Conclusion / 8.5: |
The Thermal State of a Hypersonic Vehicle Surface / 8.6: |
Heat Transport at a Vehicle Surface / 9.1: |
The Thermal State of a Vehicle Surface / 9.2: |
Aerothermpdynamic Simulation Compendium / 9.3: |
Ground-Facility Simulation / 9.3.1: |
Computational Simulation / 9.3.2: |
In-Flight Simulation / 9.3.3: |
Introduction and Delineation / 10: |
Normal Shock Wave / 10.1.2: |
Oblique Shock Wave / 10.1.4: |
Bow Shock Total Pressure Loss: Restitution of Parameters of a One-Dimensional Surface Flow / 10.1.5: |
The Compressibility Factor Z / 10.1.6: |
Transport Properties / 10.1.7: |
Formulas for Stagnation Point Heating / 10.3: |
Flat Surface Boundary Layer Parameters Based on the Reference-Temperature/Enthalpy Concept / 10.4: |
Reference-Temperature/Enthalpy Concept / 10.4.1: |
Boundary Layer Thicknesses Over Flat Surfaces / 10.4.2: |
Wall Shear Stress and Thermal State at Flat Surfaces / 10.4.3: |
Virtual Origin of Boundary Layers at Junctions / 10.4.4: |
Solution Guide and Solutions of the Problems / 11: |
Problems of Chapter 2 / 11.1: |
Problems of Chapter 3 / 11.2: |
Problems of Chapter 4 / 11.3: |
Problems of Chapter 5 / 11.4: |
Problems of Chapter 6 / 11.5: |
Problems of Chapter 7 / 11.6: |
Problems of Chapter 8 / 11.7: |
The Governing Equations of Aerothermodynamics / Appendix A: |
Governing Equations for Chemical Non-Equilibrium Flow / A.1: |
Equations for Excitation of Molecular Vibrations and Electron Modes / A.2: |
Excitation of Molecular Vibrations / A.2.1: |
Electron Modes / A.2.2: |
Vector Form of Navier-Stokes Equations Including Thermal Non-Equilibrium / A.3: |
The Earth's Atmosphere / Appendix B: |
Constants, Units and Conversions / Appendix C: |
Constants and Air Properties / C.1: |
Units and Conversions / C.2: |
Symbols / Appendix D: |
Latin Letters / D.1: |
Greek Letters / D.2: |
Indices / D.3: |
Upper Indices / D.3.1: |
Lower Indices / D.3.2: |
Other Symbols / D.4: |
Glossary, Abbreviations, Acronyms / Appendix E: |
Glossary / E.1: |
Abbreviations, Acronyms / E.2: |
Permissions |
Name Index |
Subject Index |
Introduction / 1: |
Three Reference Classes of Hypersonic Vehicles / 1.1: |
Aerothermodynamics and the Definition and Development of Flight Vehicles / 1.2: |