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Posts
- Category: Theoretical and Applied Aerodynamics (continued)
- Viscous Hypersonic Flows
- Slender Body at Angle of Attack, Bow Shocks Around Blunt Bodies and Numerical Simulations of Hypersonic Inviscid Flows
- Cole’s Slender Body Theory of Newtonian Flow
- Newtonian Flows
- Similarity Solutions for Power Law Bodies
- Formulation of the Full and Reduced Problems in Terms of Stream Functions
- Unified Supersonic-Hypersonic Small Disturbance Theory
- Unsteady Hypersonic Flows
- Unsteady Analogy
- Power Series Expansion of Pressure Coefficients
- Inviscid Theories of Hypersonic Flows
- Regimes of Compressible Flow
- Introduction to Hypersonic Flows
- . Conclusion
- Classical Versus Canard Configurations
- Trimming the Glider for Maximum Distance
- Winglet Design
- Static Stability
- Longitudinal Equilibrium
- Acceleration Phase
- Rapid Prototyping
- Aerodynamic Coefficients for the Fuselage
- Linear Model for the Tail
- Model of a Classical Wing/Tail Configuration
- Glider and Airplane Design
- Problems
- Propellers
- Perspectives
- Hybrid Method
- Validation
- Tower Interference Model
- . Effect of Yaw
- Unsteady Flow Simulation
- Validation
- Algorithm for High Incidences—Regularization of the Solution
- Analysis of the Flow Past a Given Rotor
- Viscous Correction
- Discretization
- Aerodynamic Design of a Rotor Blade—Betz Minimum Energy Condition
- Wake Equilibrium Condition
- Forces and Moment
- Biot-Savart Law—Induced Velocities
- Adimensionalization—Discretization of the Vortex Sheets
- Vortex Model and Strip Theory—The Goldstein Model
- General 1-D Conservation Theorems—Actuator Disk Theory
- Horizontal Axis Wind Turbine
- Darrieus Rotor
- Savonius Rotor
- Aerodynamics Forces—Lift and Drag
- Wind Turbine and Propeller Aerodynamics—Analysis and Design
- Viscous/Inviscid Interaction Procedures Based on Domain Decomposition Techniques
- Coupling Numerical Solutions of Partial Differential
- Coupling the Numerical Solution of the Partial Differential Equations of the Viscous Flow with the Integral Equations of the Outer Inviscid Flows
- Coupling Euler Calculations with Boundary Layer Integral Momentum Equations
- Coupling the Numerical Solution of the Partial Differential Equations of the Inviscid Flow with Integral Equations of Boundary Layers
- Analysis of Incompressible Flows over Thin Airfoils Using Integral Momentum Equation for Boundary Layer
- Coupling Integral Formulations of both Inviscid and Viscous Flow Regions
- Viscous/Inviscid Interaction Procedures Based on Displacement Thickness Concept
- Viscous/Inviscid Interaction Procedures
- Summary of Chapter 8
- Three Dimensional Boundary Layers
- Von Karman Integral Momentum Equation
- Flow Past a Wedge (Falkner/Skan)
- Blasius Solution for the Flat Plate (No Pressure Gradient)
- Historical and Classical Works
- Determination of Drag
- Boundary Layer Equations for Compressible Flows We use order of magnitude analysis to simplify the energy equation. The results are unchanged for the other equations:  
- Energy Equation for Compressible Viscous Flows
- Compressible Viscous Fluid Flow
- Boundary Layer Thicknesses
- Numerical Method for the Solution of Boundary Layer Equations
- Boundary Layer over a Flat Plate
- Laminar Boundary Layer Theory (Prandtl 1904)
- Viscous Stresses in 2-D (Cartesian Coordinates)
- Vorticity Versus Strain Rate in 2-D
- Viscous Fluid Flow and Laminar Boundary Layers
- Summary of Chapter 7
- Rectangular Wings at Angle of Attack
- Conical Flow Past a Delta Wing
- Small Disturbance Approximations for Flows Over a Cone
- Conical Flows
- Supersonic Area Rule
- Slender Bodies with General Cross Sections
- Swept and Oblique Wings
- Low Aspect Ratio Flat Wings
- Lift and Induced Drag of a Body of Revolution at Angle of Attack
- Axisymmetric Flows and Slender Body Theories
- Analysis Problem
- Summary of Chapter 6
- Transonic Lifting Line Theory
- Wings in Transonic Flows
- Wings in Supersonic Flows
- General Wings in Subsonic and Supersonic Flows
- Rectangular Wings
- Lifting Problem
- Supersonic Flow Over Moderate Aspect Ratio Wings
- Symmetric Problem in Subsonic Flow
- Compressible Flow Over Moderate Aspect Ratio Wings
- Incompressible Flow Over Moderate Aspect Ratio Wings: The Vortex Lattice Method
- Nonlinear Lift Curve and Viscous Correction