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| Fluid Properties | |
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| Concept of a Fluid | |
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| Fluid as a Continuum | |
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| Fluid Properties | |
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| Pressure Variation in a Static Fluid Medium | |
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| The Standard Atmosphere | |
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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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| 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 | |
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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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| 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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| 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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| 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). Thin, Cambered Airfoil | |
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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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| Incompressible Flows 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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| 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 Flow in a Variable-Area | |
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| Characteristic Equations and Prandtl-Meyer Flow | |
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| Shock Waves | |
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| Viscous Boundary Layer | |
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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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| Swept Wings at Transonic Speeds | |
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| Forward Swept Wing | |
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| Transonic Aircraft | |
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| Two-Dimensional Supersonic Flows around Thin Airfoil | |
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| Linear Theory | |
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| Second-Order Theory (Busemann's Theory). Shock-Expansion Technique | |
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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. Aerodynamic Interaction | |
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| Aerodynamic Analysis for Complete Configurations in a Supersonic Stream | |
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| Hypersonic Flows.</B | |