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Posts
- Category: AERODYNAMICS (continued)
- Discrete Vortex Method
- POINT SINGULARITY SOLUTIONS
- SOLUTIONS
- THREE-DIMENSIONAL HIGHER - ORDER ELEMENTS
- Horseshoe Vortex
- Vortex Ring
- Constant-Strength Vortex Line Segment
- Comparison of Near/Far-Field Formulas
- Constant Doublet Panel Equivalence to Vortex Ring
- Quadrilateral Doublet
- Quadrilateral Source
- THREE-DIMENSIONAL CONSTANT - STRENGTH SINGULARITY ELEMENTS
- Quadratic Doublet Distribution
- Linear Vortex Distribution
- Linear Doublet Distribution
- Linear Source Distribution
- TWO-DIMENSIONAL LINEAR - STRENGTH SINGULARITY ELEMENTS
- Constant-Strength Doublet Distribution
- Constant-Strength Source Distribution
- . TWO-DIMENSIONAL CONSTANT - STRENGTH SINGULARITY ELEMENTS
- Two-Dimensional Point Vortex
- TWO-DIMENSIONAL POINT SINGULARITY ELEMENTS
- SINGULARITY ELEMENTS AND INFLUENCE COEFFICIENTS
- Models for Wake Rollup, Jets, and Flow Separations
- ACCOUNTING FOR EFFECTS OF COMPRESSIBILITY AND VISCOSITY
- EXAMPLE: SOLUTION OF THIN AIRFOIL WITH THE LUMPED-VORTEX ELEMENT
- STEPS TOWARD CONSTRUCTING A NUMERICAL SOLUTION
- PRELIMINARY CONSIDERATIONS, PRIOR TO ESTABLISHING NUMERICAL SOLUTIONS
- AERODYNAMIC LOADS
- REDUCTION OF THE PROBLEM TO A SET OF LINEAR ALGEBRAIC EQUATIONS
- PHYSICAL CONSIDERATIONS
- Dirichlet Boundary Condition
- Neumann Boundary Condition
- THE BOUNDARY CONDITIONS
- BASIC FORMULATION
- METHODS
- FAR FIELD CALCULATION OF INDUCED DRAG
- Pressure and Force Information
- Transverse Flow Past a Slender Body of Revolution
- Axisymmetric Longitudinal Flow Past a Slender Body of Revolution
- Conclusions from Slender Wing Theory
- The Method of R. T. Jones
- Solution of the Flow Over Slender Pointed Wings
- Twisted Elliptic Wing
- General Spanwise Circulation Distribution
- The Elliptic-Lift Distribution
- The Aerodynamic Loads
- The Lifting-Line Model
- SOLUTIONS
- THIN AIRFOIL IN GROUND EFFECT
- MATCHED ASYMPTOTIC EXPANSIONS
- LEADING-EDGE SOLUTION
- SECOND-ORDER SOLUTION
- THIN-AIRFOIL PROBLEM
- PERTURBATION METHODS
- METHOD OF IMAGES
- Airfoil With Finite Trailing-Edge Angle
- Symmetric Joukowski Airfoil
- Circular Arc Airfoil
- Flow Normal to a Flat Plate
- Leading-Edge Suction
- Flat Plate Airfoil
- CONFORMAL MAPPING AND THE JOUKOWSKI TRANSFORMATION
- BLASIUS FORMULA KUTTA-JOUKOWSK1 THEOREM
- Flow in a Corner
- SIMPLE EXAMPLES
- THE COMPLEX POTENTIAL
- VARIABLES
- SUMMARY AND CONCLUSIONS FROM THIN AIRFOIL THEORY
- THE LUMPED-VORTEX ELEMENT
- AERODYNAMIC FORCES AND MOMENT ON A THIN AIRFOIL
- CLASSICAL SOLUTION OF THE LIFTING PROBLEM
- ZERO-THICKNESS AIRFOIL AT ANGLE OF ATTACK
- SMAL - DISTURBANCE FLOW OVER TWO-DIMENSIONAL AIRFOILS
- LINEARIZED THEORY OF SMALL - DISTURBANCE COMPRESSIBLE FLOW
- THE VORTEX WAKE
- THE AERODYNAMIC LOADS
- ZERO THICKNESS CAMBERED WING AT ANGLE OF ATTACK—LIFTING SURFACES
- SYMMETRIC WING WITH NONZERO THICKNESS AT ZERO ANGLE OF ATTACK
- SEPARATION OF THE THICKNESS AND THE LIFTING PROBLEMS
- THE BOUNDARY CONDITION ON THE WING
- FORMULATION OF THE PROBLEM
- SURFACE DISTRIBUTION OF THE BASIC SOLUTIONS
- SOME REMARKS ABOUT THE FLOW OVER THE CYLINDER AND THE SPHERE
- SUPERPOSITION OF A THREE - DIMENSIONAL DOUBLET AND FREE STREAM: FLOW AROUND A SPHERE
- SUPERPOSITION OF DOUBLET AND FREE SYSTEM: FLOW AROUND A CYLINDER
- SUPERPOSITION OF SOURCES AND FREE STREAM: RANKINE’S OVAL
- PRINCIPLE OF SUPERPOSITION
- BASIC SOLUTION: VORTEX
- TWO-DIMENSIONAL VERSION OF THE BASIC SOLUTIONS
- BASIC SOLUTION: POLYNOMIALS
- BASIC SOLUTION: POINT DOUBLET
- BASIC SOLUTION: POINT SOURCE
- SUMMARY: METHODOLOGY OF SOLUTION
- THE GENERAL SOLUTION, BASED ON GREEN’S IDENTITY
- EQUATIONS
- THE STREAM FUNCTION
- THE VELOCITY INDUCED BY A STRAIGHT VORTEX SEGMENT
- THE BIOT-SAVART LAW
- TWO-DIMENSIONAL VORTEX