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Posts
- Category: AERODYNAMICS (continued)
- VORTEX QUANTITIES
- UNIQUENESS OF THE SOLUTION
- SIMPLY AND MULTIPLY CONNECTED REGIONS
- BERNOULLI’S EQUATION FOR THE PRESSURE
- BOUNDARY AND INFINITY CONDITIONS
- IRROTATIONAL FLOW AND THE VELOCITY POTENTIAL
- RATE OF CHANGE OF CIRCULATION: KELVIN’S THEOREM
- RATE OF CHANGE OF VORTICITY
- FUNDAMENTALS OF INVISCID, INCOMPRESSIBLE FLOW
- SIMILARITY OF FLOWS
- FLOW WITH HIGH REYNOLDS NUMBER
- DIMENSIONAL ANALYSIS OF THE FLUID DYNAMIC EQUATIONS
- DIFFERENTIAL FORM OF THE FLUID DYNAMIC EQUATIONS
- INTEGRAL FORM OF THE FLUID DYNAMIC EQUATIONS
- FORCES IN A FLUID
- PATHLINES, STREAK LINES, AND STREAMLINES
- CHOICE OF COORDINATE SYSTEM
- DESCRIPTION OF FLUID MOTION
- Aerospace Engineering
- Category: Aerodynamics for Engineering Students
- The hovercraft
- The free motion of a rocket-propelled body
- The rocket motor
- Translational helicopter flight
- Vertical climbing flight
- The momentum theory applied to the helicopter rotor
- The performance of a blade element
- Blade element theory
- Experimental mean pitch
- Airscrew pitch
- Activity factor
- Torque coefficient
- Airscrew coefficients
- Froude's momentum theory of propulsion
- Propellers and propulsion
- Reduction of wave drag
- Reduction of form drag
- Riblets
- Compliant walls: artificial dolphin skins
- Laminar flow control by boundary-layer suction
- Reduction of skin-friction drag
- Other methods of separation control
- Control by tangential blowing
- Boundary layer control for the prevention of separation
- Movable flaps: artificial bird feathers[63]
- Gurney flaps
- Use of multi-element aerofoils on racing cars
- Fresh boundary-layer effect
- Off-the-surface recovery
- The slat effect
- Multi-element aerofoils
- Maximizing lift for single-element aerofoils
- Flow control and wing. design
- Shock-wave/boundary-layer interaction in supersonic flow
- Near-normal shock interaction with turbulent boundary layer
- Near-normal shock interaction with laminar boundary layer
- Some boundary-layer effects in supersonic flow
- Growth rate of two-dimensional wake, using the general momentum integral equation
- B. M. Jones' wake traverse method for determining profile drag
- The momentum integral expression for the drag of a two-dimensional body
- Estimation of profile drag from velocity profile in wake
- Large-eddy simulation
- The k-є method - A typical two-equation method
- Zero-equation methods
- Computational solution of turbulent boundary layers
- Computational solution of the laminar boundary-layer equations
- Transition prediction
- Computational methods
- Turbulence structure in the near-wall region
- Distribution of Reynolds stresses and turbulent kinetic energy across the boundary layer
- Formulae for local skin-friction coefficient and drag
- Regimes of turbulent wall flow
- Prandtl's mixing-length theory of turbulence
- Eddy viscosity
- Boundary-layer equations for turbulent flows
- Reynolds averaging and turbulent stress
- Laminar-turbulent transition
- Additional examples of the application of the momentum integral equation
- Mixed boundary layer flow on a flat plate with zero pressure gradient
- Conditions at transition
- Drag coefficient for a flat plate with wholly turbulent boundary layer
- Drag coefficient for a flat plate of streamwise length L with wholly laminar boundary layer
- Rate of growth of a laminar boundary layer on a flat plate
- Simplified form of the momentum integral equation
- Approximate methods for a boundary layer on a flat plate with zero pressure gradient
- An approximate velocity profile for the laminar boundary layer
- The momentum integral equation
- Cricket balls
- Golf balls
- Turbulence spheres
- Flow past cylinders and spheres
- Separation bubbles
- Boundary-layer separation
- Solution for the general case
- Solution of the boundary-layer equations for a flat plate
- Skin friction drag
- Various definitions of boundary-layer thickness
- Derivation of the laminar boundary-layer equations
- The boundary-layer equations
- Effects of an external pressure gradient