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| Preface | |
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| Why Study Aerodynamics? | |
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| Aerodynamics and the Energy-Maneuverability Technique | |
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| Solving for the Aerothermodynamic Parameters | |
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| Description of an Airplane | |
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| Summary | |
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| Problems | |
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| References | |
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| Fundamentals of Fluid Mechanics | |
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| Introduction to Fluid Dynamics | |
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| Conservation of Mass | |
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| Conservation of Linear Momentum | |
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| Applications to Constant-Property Flows | |
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| Reynolds Number and Mach Number as Similarity Parameters | |
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| Concept of the Boundary Layer | |
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| Conservation of Energy | |
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| First Law of Thermodynamics | |
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| Derivation of the Energy Equation | |
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| Summary | |
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| Problems | |
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| References | |
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| Dynamics of an Incompressible, Inviscid Flow Field | |
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| Inviscid Flows | |
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| Bernoulli's Equation | |
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| Use of Bernoulli's Equation to Determine Airspeed | |
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| The Pressure Coefficient | |
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| Circulation | |
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| Irrotational Flow | |
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| Kelvin's Theorem | |
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| Incompressible, Irrotational Flow and the Velocity Potential | |
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| Stream Function in a Two-Dimensional, Incompressible Flow | |
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| Relation between Streamlines and Equipotential Lines | |
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| Superposition of Flows | |
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| Elementary Flows | |
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| Adding Elementary Flows to Describe Flow Around a Cylinder | |
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| Lift and Drag Coefficients as Dimensionless Flow-Field Parameters | |
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| Flow Around a Cylinder with Circulation | |
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| Source Density Distribution on the Body Surface | |
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| Incompressible, Axisymmetric Flow | |
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| Summary | |
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| Problems | |
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| References | |
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| Viscous Boundary Layers | |
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| Equations Governing the Boundary Layer for a Steady, Two-Dimensional, Incompressible Flow | |
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| Boundary Conditions | |
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| Incompressible, Laminar Boundary Layer | |
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| Boundary-Layer Transition | |
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| Incompressible, Turbulent Boundary Layer | |
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| Eddy Viscosity and Mixing Length Concepts | |
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| Integral Equations for a Flat-Plate Boundary Layer | |
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| Thermal Boundary Layer for Constant-Property Flows | |
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| Summary | |
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| Problems | |
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| References | |
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| Characteristic Parameters for Airfoil and Wing Aerodynamics | |
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| Characterization of Aerodynamic Forces and Moments | |
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| Airfoil Geometry Parameters | |
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| Wing-Geometry Parameters | |
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| Aerodynamic Force and Moment Coefficients | |
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| Wings of Finite Span | |
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| Problems | |
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| References | |
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| Incompressible Flows Around Airfoils of Infinite Span | |
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| General Comments | |
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| Circulation and the Generation of Lift | |
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| General Thin-Airfoil Theory | |
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| Thin, Flat-Plate Airfoil (Symmetric Airfoil) | |
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| Thin, Cambered Airfoil | |
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| Laminar-Flow Airfoils | |
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| High-Lift Airfoil Sections | |
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| Multielement Airfoil Sections for Generating High Lift | |
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| High-Lift Military Airfoils | |
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| Summary | |
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| Problems | |
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| References | |
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| Incompressible Flow About Wings of Finite Span | |
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| General Comments | |
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| Vortex System | |
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| Lifting-Line Theory for Unswept Wings | |
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| Panel Methods | |
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| Vortex Lattice Method | |
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| Factors Affecting Drag Due-to-Lift at Subsonic Speeds | |
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| Delta Wings | |
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| Leading-Edge Extensions | |
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| Asymmetric Loads on the Fuselage at High Angles of Attack | |
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| Flow Fields for Aircraft at High Angles of Attack | |
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| Unmanned Air Vehicle Wings | |
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| Summary | |
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| Problems | |
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| References | |
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| Dynamics of a Compressible Flow Field | |
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| Thermodynamic Concepts | |
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| Adiabatic Flow in a Variable-Area Streamtube | |
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| Isentropic How in a Variable-Area Streamtube | |
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| Converging-diverging Nozzles | |
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| Characteristic Equations and Prandtl-Meyer Flows | |
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| Shock Waves | |
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| Viscous Boundary Layer | |
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| Shock-Wave/Boundary-Layer Interactions | |
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| Shock/Shock Interactions | |
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| The Role of Experiments for Generating Information Defining the Flow Field | |
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| Comments About the Scaling/Correction Process(es) for Relatively Clean Cruise Configurations | |
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| Summary | |
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| Problems | |
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| References | |
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| Compressible, Subsonic Flows and Transonic Flows | |
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| Compressible, Subsonic Flow | |
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| Transonic Flow Past Unswept Airfoils | |
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| Wave Drag Reduction by Design | |
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| Swept Wings at Transonic Speeds | |
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| Transonic Aircraft | |
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| Summary | |
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| Problems | |
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| References | |
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| Two-Dimensional, Supersonic Flows Around Thin Airfoils | |
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| Linear Theory | |
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| Second-Order Theory (Busemann's Theory) | |
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| Shock-Expansion Technique | |
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| Summary | |
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| Problems | |
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| References | |
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| Supersonic Flows Over Wings and Airplane Configurations | |
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| General Remarks About Lift and Drag | |
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| General Remarks About Supersonic Wings | |
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| Governing Equation and Boundary Conditions | |
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| Consequences of Linearity | |
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| Solution Methods | |
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| Conical-Flow Method | |
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| Singularity-Distribution Method | |
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| Design Considerations for Supersonic Aircraft | |
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| Some Comments About the Design of the SST and of the HSCT | |
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| Slender Body Theory | |
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| Base Drag | |
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| Aerodynamic Interaction | |
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| Aerodynamic Analysis for Complete Configurations in a Supersonic Free Stream | |
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| Summary | |
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| Problems | |
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| References | |
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| Hypersonic Flows | |
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| The Five Distinguishing Characteristics | |
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| Newtonian Flow Model | |
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| Stagnation Region Flow-Field Properties | |
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| Modified Newtonian Flow | |
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| High L/D Hypersonic Configurations-Waveriders | |
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| Aerodynamic Heating | |
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| A Hypersonic Cruiser for the Twenty-First Century? | |
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| Importance of Interrelating CFD, Ground-Test Data, and Flight-Test Data | |
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| Boundary-Layer-Transition Methodology | |
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| Summary | |
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| Problems | |
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| References | |
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| Aerodynamic Design Considerations | |
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| High-Lift Configurations | |
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| Circulation Control Wing | |
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| Design Considerations for Tactical Military Aircraft | |
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| Drag Reduction | |
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| Development of an Airframe Modification to Improve the Mission Effectiveness of an Existing Airplane | |
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| Considerations for Wing/Canard, Wing/Tail, and Tailless Configurations | |
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| Comments on the F-15 Design | |
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| The Design of the F-22 | |
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| The Design of the F-35 | |
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| Summary | |
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| Problems | |
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| References | |
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| Tools for Defining the Aerodynamic Environment | |
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| Computational Tools | |
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| Establishing the Credibility of CFD Simulations | |
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| Ground-Based Test Programs | |
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| Flight-Test Programs | |
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| Integration of Experimental and Computational Tools: The Aerodynamic Design Philosophy | |
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| Summary | |
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| References | |
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| The Equations of Motion Written in Conservation Form | |
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| A Collection of Often Used Tables | |
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| Answers to Selected Problems | |
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| Index | |
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| Credits | |