Flight Controls Flashcards
It is more convenient to study the coefficients of the various moments of each control, rather than their total value.
The abbreviation for pitch movement is …
Cm
It is more convenient to study the coefficients of the various moments of each control, rather than their total value.
The abbreviation for roll movement is …
Cl
It is more convenient to study the coefficients of the various moments of each control, rather than their total value.
The abbreviation for yaw movement is …
Cn
what is the secondary effect of elevator input?
none
what is the secondary effect of rudder input?
roll
what is the secondary effects of aileron input?
adverse yaw
sideslip with bank
what is the purpose of a trim tab?
how does its position change when the main control moves?
to hold the main control in a position in flight so that the aircraft will maintain its attitude if flown hands off
Does not change its set position relative to the main control surface as the main control moves
what is the purpose of balance tabs?
how does it position change when the main control moves?
assists the pilot in moving the controls
move in the opposite direction to the main control surface do assist its movement
what is a servo tab?
Pilot’s control input goes directly to the tab, which moves the main control through aerodynamic forces – no connection at all between the control column and the control surface
what is a spring tab?
A spring is introduced to the control linkage to change stick forces at high speed. The only connection between the linkage and the control surface is a spring, which at low speed will move the control surface without any tab movement
But when the force required increases at high IAS, the spring stretches and deflection of the tab begins, reducing stick forces at high speed
what must you be careful of with spring tab control locks?
must be externally locked as the control surface would still be able to move due to the spring stretching
also movement of the control stick does not confirm that the control lock is out because the spring will allow movement of the stick while the control surface is locked in position
what are anti-balance tabs used for?
how do they move in relation to the main control surface?
Used if control forces are too light
Deflect in the same direction as the main control to increase the control forces
what causes adverse yaw?
Induced drag increases on upgoing wing, and reduces on down going wing, thus creating a yaw in the wrong direction
what are differential ailerons and what are they used for?
down going aileron is deflected less than the up going aileron re-balancing the drag to couteract adverse yaw?
what are frise ailerons and what are they used for?
have a projection on their leading edge that extends down below the wing when the aileron deflects upwards, increasing drag on the down going wing to counteract adverse yaw