ACFT - Effects of Controls & Stability Flashcards
Fixed wing aircraft Components diagram (Part 1) (5)
Fixed wing aircraft Components diagram (Part 2) (3)
Fixed wing aircraft Components diagram (Part 3) (2)
Helicopter Components diagram (Part 1) (7)
Helicopter Components diagram (Part 2) (4)
What 3 dimensions can an aircraft move in? (3)
All 3 axes pass through the aircraft’s centre of gravity
What Axis does the aircraft Pitch affect? (1)
Lateral Axis
What Axis does the aircraft Roll affect? (1)
Longitudinal Axis
What Axis does the aircraft Yaws affect? (1)
Vertical Axis
What the components of the Empennage? (4)
- Horizontal stabiliser
- Elevators
- Tail fin
- Rudder
What is the Tailplane? (3)
- AKA Horizontal stabiliser
- An aerofoil
- Assists longitudinal stability (Up/down pitching motion)
What is the Elevator? (2)
- Moving section at the rear of the stabiliser
- Activated by pulling or pushing the control column forward or backwards
What is a Tail fin? (2)
- Aerofoil
- Helps to give the aircraft directional stability by preventing yawing
What is the Rudder? (2)
- Controls the aircraft’s Yaw
- Points the nose of the aircraft in the intended direction by altering the shape of the aerofoil and thereby changing the forces generated on it
What are Ailerons? (3)
- Small hinged sections on the outer part of each wing
- Move in opposite directions (Up / down)
- Results in a rolling motion around the longitudinal axis, acting through the centre of gravity
Ailerons, Control Yoke, Elevators, Rudder diagram
What do Modern aircraft have to assist / power the control surfaces? (1)
Hydraulic systems
How many redundancies do hydraulic systems usually have on modern aircraft? (1)
Usually 3
(Redundancy systems or electrical powered back up systems)
What is a “Fly by wire”? (1)
A system that replaces the conventional manual flight controls of an aircraft with an electronic interface
What is the secondary effect when the aircraft rolls? (2)
- Resultant lift reduces because gravity always acts vertically towards the Earth
- The pilot counteracts the loss of lift in a turn by applying more elevator (Applying more elevator increases the rate of turn)
What is Adverse Yaw? (1)
The natural and undesirable tendency for an aircraft to yaw in the opposite direction of a roll
What is Adverse Roll? (1)
When a pilot applies rudder to yaw the nose of the aircraft, the starboard wing will generate fractionally more lift as it travels slightly faster relative to the airmass
Vee tail aircraft example
Elevon aircraft example