Ch 3A - Four Forces of Flight Flashcards
Four forces acting on an airplane
Life, weight, thrust, and drag
Four forces are in equilibrium
During unaccelerated flight
Force created by the effects of airflow as it passes over and under the wing
Lift
The airplanes wing shape is designed to take advantage of
Newton’s laws and Bernoulli’s principles
Bernoulli’s principle
Increase in speed of air on the top of an airfoil produces a drop in pressure and this lowered pressure is a component of total lift. The decrease in speed of air on the bottom of the airfoil produces an increase in pressure, providing the main component of total lift
Newton’s third law of motion
The reaction to downwash causes an upward reaction
Design factors that affect a wings lifting capability
Planform, camber, aspect ratio, wing area
A stall is caused by
The separation of airflow from the wings upper surface, and always occurs at an airplanes critical angle of attack regardless of airspeed, attitude or weight
Total lift depends on
The combined effects of airspeed and angle of attack
When speed decreases
ou must increase the angle of attack to maintain the same amount of lift
Flaps
Increase lift and drag by increasing the wings effective camber and changing the chord line that increases the angle of attack
Flap types
Plain(hinge), split(only lower hinged), slotted(plane w/gap) and fowler(slide out w/gap)
Weight
Force of gravity that acts vertically through the center of gravity of the airplane towards the center of the earth
Thrust
Forward-facing force that opposes drag and propels the airplane
Drag
Acts in opposition to the direction on flight and opposes thrust, limits the forward speed of an airplane