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Posts
- Category: BASIC AERODYNAMICS (continued)
- Pressure Gradients and Boundary-Layer Profiles: A Qualitative Assessment
- Boundary Layer with a Streamwise Pressure Gradient
- Boundary-Layer Displacement Thickness
- Boundary-Layer Thickness
- Numerical Solution of the Blasius Equation by Finite Differences
- The z-Velocity Component in the Boundary Layer
- Comparison of Theoretical Solution to Experimental Data
- Application of the Similarity Method
- Incompressible Boundary-Layer Theory
- Orders of Magnitude
- Derivation of the Boundary-Layer Equations
- The Prandtl Boundary-Layer Equations
- Role of the Reynolds Number
- Decay of a Potential Vortex
- Steady, Incompressible Flow Between Two Semi-Infinite Parallel Plates
- Exact Solutions of the Navier-Stokes Equations
- Boundary Conditions for Viscous Flows
- Navier-Stokes Equations for Incompressible Flow
- Navier-Stokes Equations
- Viscous Incompressible Flow
- Numerical Methods
- Flow Past a General Body of Revolution
- Superposition of Uniform Flow and a Source Flow
- Elementary Solutions for the Stream Function in Axisymmetric Flow
- Incompressible Flow around a Sphere
- Three-Dimensional Point Source at the Origin of Coordinates
- Defining Equation for the Stream Function
- Defining Equation for the Velocity Potential
- The Momentum Equation
- Axisymmetric Continuity and Momentum Equations
- Axisymmetric, Incompressible Flow around a Body of Revolution
- Strakes and Canards
- Leading-Edge Vortex Flap
- Polhamus Method
- Vortex Lift
- Winglets
- Ground Effect
- Aerodynamic Strip Theory
- Comments on Wing-Analysis Methods
- Vortex-Lattice Method
- Vortex Panel Method
- Wing-Panel Methods
- Wing Drag
- Remarks on Lift and Drag of a Finite Wing from Lifting-Line Theory
- Wing Geometry Required for Elliptical Loading, Lifting-Line Theory
- Forces on an Arbitrary Finite Wing from Lifting-Line Theory
- Spanwise-Lift Distribution on an Arbitrary Wing by Lifting-Line Theory
- Wing Twist
- Lift and Induced Drag
- Induced Angle of Attack
- Downwash
- Assumptions of the Lifting-Line Theory
- Lifting-Line Concept
- Prandtl Lifting-Line Theory
- The Biot-Savart Law
- Incompressible Flow about Wings of Finite Span
- Inverse Methods of Solution
- Distributed Singularity (Panel) Numerical Methods
- Thin Airfoil with a Flap
- Agreement of Thin-Airfoil Theory with Experimental Data
- Center of Pressure
- Aerodynamic Center
- Moment Coefficient
- The Symmetrical Thin Airfoil
- Vortex-Sheet Representation of a Thin Airfoil
- Vortex-Sheet Representation of an Airfoil
- The Vortex Sheet
- Distribution of Singularities on the Surface of a Body
- Thin-Airfoil Theory
- NACA Six-Digit Airfoils
- NACA Four-Digit Airfoils
- The NACA Series of Airfoils
- Mathematical Approach
- Two-Dimensional Airfoil Behavior
- Airfoil-Shape Parameters
- Two-Dimensional Airfoils
- The Starting Vortex: Kelvin’s Theorem
- The Kutta Condition
- The Kutta-Joukouski Theorem
- Uniform Flow Plus Doublet Plus Vortex: Flow Around a Lifting Cylinder
- Uniform Flow Plus Source-Sink Pair
- Superposition of Elementary Solutions
- Doublet (or Dipole)
- Source-Sink Pair
- Source Flow
- Elementary Solutions
- Solving Laplace’s Equation
- Solving the Conservation Equations
- Special Solutions of the Conservation Equations
- Stream Function and Velocity Potential
- Circulation
- Vorticity and Curl
- Angular Velocity and Strain
- Streamline and Stream Tube
- Basic Building Blocks
- 4 Fundamentals of Steady, Incompressible, Inviscid Flows
- Examples of the Art of Approximation
- Practical Methods of Problem Solution
- Solution Procedures
- Boundary Conditions