Exam 100% Solved Correctly
Pitching - Answer- rotation around the lateral axis (and is related to longitudinal stability)
Rolling - Answer- rotation around the longitudinal axis
Yawing - Answer- rotation around the normal (vertical axis)
To pitch up - Answer- back pressure on control column = elevator moves up + negative
camber of tailplane/elevator increases (to provide downforce)
Trimmable horizontal stabiliser (forward CG) - Answer- requires stabiliser to produce
more downforce therefore lower stabiliser AoA needed
Trimmable horizontal stabiliser (aft CG) - Answer- less nose down pitching moment
from the wing - stabiliser does not need to produce as much down force - so stabiliser
leading edge higher
In trim - Answer- elevator will have no deflection in relation to the aerofoil
Positive Angle of Incidence (Stabiliser) - Answer- stabiliser will give greater nose down
pitching moments
Internal Balance - Answer- flexible seal - uses pressure differentials within a sealed
cavity forward of the hinge line
Horn balance - Answer- part of control surface located ahead of the hinge line to
protrude in the airflow
Balance tab - Answer- deflect in opposite direction to main control
Anti-balance tab - Answer- deflect in same direction to main control, for light control
forces to increase control forces
Trim tab - Answer- Once set a trim tab does not change its position relative to the
control surface when that surface moves
Servo tab - Answer- pilot's control input goes directly to the tab and control deflection
carried out by the aerodynamic forces generated by the tab
Spring tab - Answer- spring introduced into the control linkage to change stick forces at
high speed. At high speeds, the spring stretches and deflection of the tab begins