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Posts
- Category: Theoretical and Applied Aerodynamics (continued)
- Numerical Solution of Prandtl Integro-Differential Equation
- Extension of the Theory to Non-straight Lifting Lines
- Example of Wing Loading with Upwash
- Pitching Moment
- Local and Global Lift Coefficients
- . Design of an Ideal Wing
- Induced Drag for Non-ideal Wings
- Prandtl Lifting Line Theory (Incompressible Flow)
- Drag
- Lift
- Forces
- Two-Dimensional and Three-Dimensional Vorticity epresentations
- Fundamental Feature of the Flow Past Finite Wings: The Vortex Sheet
- Flow Past Thin Wings
- Small Disturbance Theories
- . Wing Geometric Parameters
- Flow Past Large and Moderate Aspect Ratio Wings
- Falling Plate over Flat Surface
- Problems
- Summary of Chapter 5
- The Transonic Small Disturbance Equation
- Unsteady Compressible Flows
- Example: Pitching NACA0012
- Example: Plunging Plate
- Unsteady Flow Past Thin Airfoils: Far Field Condition for Potential
- Unsteady Flow Past Thin Cambered Plates: Forces and Moment
- Inviscid, Unsteady Flows Past Airfoils
- Problems
- Summary of Chapter 4
- Supersonic Flow Adjacent to Uniform Flow Region
- A Useful Nozzle Flow Solution
- Murman-Cole Scheme
- Forces and Moment
- Boundary Conditions
- Transonic Small Disturbance Theory
- Limit of Validity of Linearized Theories
- Center of Pressure
- Moment
- Forces
- Jump Conditions: Shock and Expansion Waves
- Linearized Supersonic Flow
- Prandtl-Glauert Transformation
- Linearized Compressible Flow Potential Equation
- Governing Equations
- Inviscid, Compressible Flow Past Thin Airfoils
- Problems
- Summary of Chapter 3
- Numerical Solution of the Fundamental Integral Equation
- A Family of Profiles with Minimum Pressure Gradient
- Example of Design Problem
- . or in terms of the dimensionless coefficients
- Center of Pressure
- Moment
- Forces
- Example: Parabolic Plate
- Example: Flat Plate
- Solution of the Fundamental Integral Equation
- Lifting Problem
- The Symmetric Problem
- Decomposition into Symmetric and Lifting Problems
- Linearization of the Pressure Coefficient
- Linearization of the Tangency Condition
- Small Disturbance Linearization Method
- Examples of Camber and Thickness Distributions
- Profile at Incidence
- Inviscid, Incompressible Flow Past Thin Airfoils
- Problems
- Summary of Chapter 2
- Joukowski Airfoil at Incidence
- Circular Arc
- The Flat Plate at Incidence
- The Ellipse at Incidence
- Special Cases of Joukowski Airfoils
- Center of Pressure—Aerodynamic Center
- The Kutta-Joukowski Condition
- Flow Past Arbitrary Airfoils
- Flow Past a Circular Cylinder
- Global Integrals
- Superposition of Elementary Solutions
- Potential Vortex
- Doublet
- Source and Sink
- Elementary Solutions
- . Other Formulations
- Boundary Conditions
- Inviscid, Incompressible Flow Past Circular Cylinders and Joukowski Airfoils
- Description of the Book Content
- Discussion of Mathematical Models
- Definitions and Notations
- Theoretical and Applied Aerodynamics
- Category: Transport
- Category: Uncategorized
- Category: UNSTEADY AERODYNAMICS, AEROACOUSTICS AND AEROELASTICITY OF TURBOMACHINES