26-04-2011, 12:41 PM
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TERMINOLOGIES USED
ANGLE OF ATTACK
CAMBER
LEADING EDGE
TRAILING EDGE
CHORD
BOUNDARY LAYER
Angle of attack
AIROFOIL
BOUNDARY LAYER
Cause for the turbulence
Physical significance of Reynolds Number
Typical Boundary layer thickness
FORCES ACTING ON AIRCRAFT
HOW AEROFOIL PRODUCES LIFT?
Pressure distribution around the airfoil
FLOW PAST AN AEROFOIL
FLOW SEPERATION
(pressure drag)
EULER’S EQUATION
BERNOULLI’S EQUATION
Application of Bernoulli's principle
SIGNIFICANCE OF DIMENSIONAL ANALYSIS IN AERODYNAMICS
Pi THEOREM
MACH NUMBER EFFECT
SHOCK CONE
SHOCK WAVES
WING TIP VORTICES
Hazards of wing tip vortices
TAKE OFF FORCES
Expression for the forces during take off
FORCES DURING LANDING
FORCES ON AIRCRAFT DURING TURN
FORCES DURING A LOOP
Three Rotations and The Control Surfaces Which Produce Them
TERMINOLOGIES USED
ANGLE OF ATTACK
CAMBER
LEADING EDGE
TRAILING EDGE
CHORD
BOUNDARY LAYER
Angle of attack
AIROFOIL
BOUNDARY LAYER
Cause for the turbulence
Physical significance of Reynolds Number
Typical Boundary layer thickness
FORCES ACTING ON AIRCRAFT
HOW AEROFOIL PRODUCES LIFT?
Pressure distribution around the airfoil
FLOW PAST AN AEROFOIL
FLOW SEPERATION
(pressure drag)
EULER’S EQUATION
BERNOULLI’S EQUATION
Application of Bernoulli's principle
SIGNIFICANCE OF DIMENSIONAL ANALYSIS IN AERODYNAMICS
Pi THEOREM
MACH NUMBER EFFECT
SHOCK CONE
SHOCK WAVES
WING TIP VORTICES
Hazards of wing tip vortices
TAKE OFF FORCES
Expression for the forces during take off
FORCES DURING LANDING
FORCES ON AIRCRAFT DURING TURN
FORCES DURING A LOOP
Three Rotations and The Control Surfaces Which Produce Them