Effects of Controls Flashcards
(15 cards)
Primary Flight Controls
Consist of Elevator, Ailerons and rudder
Secondary flight controls
Consist of wing flaps and trim system
Elevators
– Primary control for changing the pitch attitude of an airplane
– Controls pitch about the lateral axis
– Controlled by pushing and pulling the yoke
Rudders
– Primary control for yawing the aircraft
– Controls movement of the aircraft about
its vertical axis
– Controlled by rudder pedals
Ailerons
– Primary control for banking the aircraft
– Controls roll about the longitudinal axis
– Controlled by turning the yoke
Adverse Yaw
– Yaw produced on the upgoing wing that yaws the aircraft’s nose AWAY from the turn.
– Is caused by higher induced drag on the outside wing, which is producing more lift.
How adverse yaw is countered by differential ailerons?
➢With differential ailerons, one aileron is raised a greater distance than the other aileron is lowered for a given movement of the control wheel or control
How adverse yaw is countered by rudder?
The main purpose of a rudder in flight is to counter adverse yaw by keeping the aircraft coordinated
How adverse yaw is countered by Friss-type ailerons?
With a Frise-type aileron, when pressure is applied to the control wheel or control stick, the aileron that is being raised pivots on an offset hinge projects the leading edge of the aileron into the airflow and creates drag.
Trim Tabs
Reduces the stick forces or control force so that the pilot can maintain any yaw, pitch or roll without further control unit.
Flaps
– Flaps are the most common high-lift devices used on aircraft.
–These surfaces, which are attached to the
trailing edge of the wing, increase both lift
and induced drag for any given AOA.
Importance of Flaps
*Shorter takeoff roll
*Slower landing speeds
*Steeper descent path
*Better view of the runway on approach
Effects of Flaps in stall speeds
Lowering the flaps will decrease the stalling speed of the airplane
Types of Flaps
- Plain flap
- Split flap
- Slotted flap
- fowler flap
- slotted fowler flap
Flaps lift and drag percentage when deployed
Flaps 10 - 20% lift, 5 % drag
Flaps 20 - 20% lift, 20% drag
Flaps 30 - 10% lift, 35% drag