review chapter 12
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Review Chapter 12. Fundamental Flight Maneuvers. Straight and Level Turns Climbs Descents. Turns. The horizontal component of lift. Load Factor and Turns The relationship between angle of bank , load factor, and stall speed is the same for all airplanes. Turns. - PowerPoint PPT PresentationTRANSCRIPT
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Review Chapter 12
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Fundamental Flight Maneuvers• Straight and Level• Turns• Climbs • Descents
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Turns• The horizontal component of lift.• Load Factor and Turns• The relationship between angle of
bank , load factor, and stall speed is the same for all airplanes
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Turns• Banking - increases stall speed• To increase the rate of turn and at
the same time decrease the radius - increase bank and decrease speed
• To maintain altitude - increase angle of attack
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Four Aerodynamic Forces• Lift• Thrust• Drag• Weight• When are they in equilibrium?
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Lift• Perpendicular to the relative wind• Induced drag is a by-product of lift• In theory if the angle of attack and
other factors remain constant double the speed - four times the lift
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Controlling Lift• Increase airspeed• Change the angle of attack• Change the shape of the airfoil• Change the total area of the
wings
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Bernoulli’s Principle• As the velocity of a fluid
increase, its internal pressure decreases
• High pressure under the wing and lower pressure above the wing’s surface
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Angle of Attack• Directly controls the distribution
of pressure acting on a wing. By changing the angle of attack, you can control the airplane’s lift, airspeed and drag.
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Angle of Attack• Angle of attack at which a wing
stalls remains constant regardless of weight, dynamic pressure, bank angle or pitch attitude.
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Stalls• Stall speed is not a fixed value• Stall speed is affected by weight,
load factor and power• Frost can cause a wing to stall at a
lower than normal angle of attack
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Flaps• Plain• Split• Slotted• Fowler
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Ground Effect• Within one wingspan of the
ground• An airplane leaving ground effect
will experience an increase in what kind of drag?
• Induced
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Drag• What kind of drags rate of
increase is proportional to the square of the airspeed?
• Parasite Drag• What kinds of drag make up
parasite Drag
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Drag• Form• Interference• Skin Friction
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Load Factor• Ratio between the lift generated
by the wings at any given time divided by the total weight of the airplane.
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Load Factor• A heavily loaded plane stalls at a
higher speed than a lightly loaded airplane.
• It needs a higher angle of attack to generate required lift at any given speed than when lightly loaded.
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Aircraft Stability• Achieved by locating the center
of gravity slightly ahead of the center of lift
• Need a tail down force on the elevator
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Aircraft Stability• In light planes, recovery from a
spin may be difficult with a rearward CG
• Longitudinal stability involves motion about the lateral axis and is controlled by the elevator
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Density Altitude• High• Hot • Humid
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Surface Winds• Headwind or tailwind component
–a 10 knot headwind might improve performance by 10%
–a 10 knot tailwind might degrade performance by 40%
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Performance Charts• Experience Test Pilots• Factory new Airplanes• Repeated Tests using Best
Results• Format -Table -Graphic
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Cruise Charts• Range is the distance an airplane
can travel with a given amount of fuel
• Endurance is the length of time the airplane can remain in the air
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Cruise Charts• Maximum range is at L/Dmax or
best glide speed• Maximum endurance is about
76% or best glide speed• Generally close to stall speed
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Excessive Weight• Higher takeoff speed• Longer takeoff run• Reduced rate and angle of climb• Lower maximum altitude
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Excessive Weight• Shorter range and endurance• Reduced cruise speed and
maneuverability• Higher stall speed• Higher landing speed and longer
landing roll
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Forward CG Effects• Higher takeoff speed and ground
roll• Reduced rate and angle of climb• Lower maximum altitude• Reduced maneuverability
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Forward CG Effects• Higher stalling speed• Reduction in performance
caused by increased tail-down loading
• Reduced pitch authority
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Beyond Aft CG Effects• Decreased stability and increased
susceptibility to over control• Increased risk of stalls and spins
of which recovery may be difficult or impossible
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Weight Shift Computations
Weight of Cargo Moved Distance CG moves
Airplane weight = Distance Between Arm locations