The ______ ________ runs the length of an airfoil from the root to the tip and is the main
spanwise member of the structure that carries the aerodynamic load to the fuselage
structure.
Give this one a try later!
Wing Spar
what are the four forces acting on a helicopter rotor?
Give this one a try later!
, -Gravity
-Centrifugal Force
-Lift
-Drag
_______________ is the state of flight where relative winds turns the main rotor system as
opposed to the engine power turning the rotor
Give this one a try later!
Autorotation
__________ is the characteristic of an airplane in flight that causes it to return to a
condition of equilibrium
Give this one a try later!
Stability
__________ __________ are installed as a simple method to stop or reduce the spanwise flow
of air on a wing
Give this one a try later!
Wing Fences
, _______ ________ __________ are created by the difference in pressure between the upper and
lower surfaces of a wing that cause air to still over the wing tip
Give this one a try later!
Wing tip vortices
A _______________ gauge is used to ensure that a cable terminal is properly swaged onto a
cable end
Give this one a try later!
Go/No-Go Gauge
The ______________ axis is the straight line passing through the fuselage from the nose to
tail. The motion about this access is referred to as _____
Give this one a try later!
Longitudinal, Roll
the pitch of the tail rotor is controlled by ________ operated by the pilot
Give this one a try later!
spanwise member of the structure that carries the aerodynamic load to the fuselage
structure.
Give this one a try later!
Wing Spar
what are the four forces acting on a helicopter rotor?
Give this one a try later!
, -Gravity
-Centrifugal Force
-Lift
-Drag
_______________ is the state of flight where relative winds turns the main rotor system as
opposed to the engine power turning the rotor
Give this one a try later!
Autorotation
__________ is the characteristic of an airplane in flight that causes it to return to a
condition of equilibrium
Give this one a try later!
Stability
__________ __________ are installed as a simple method to stop or reduce the spanwise flow
of air on a wing
Give this one a try later!
Wing Fences
, _______ ________ __________ are created by the difference in pressure between the upper and
lower surfaces of a wing that cause air to still over the wing tip
Give this one a try later!
Wing tip vortices
A _______________ gauge is used to ensure that a cable terminal is properly swaged onto a
cable end
Give this one a try later!
Go/No-Go Gauge
The ______________ axis is the straight line passing through the fuselage from the nose to
tail. The motion about this access is referred to as _____
Give this one a try later!
Longitudinal, Roll
the pitch of the tail rotor is controlled by ________ operated by the pilot
Give this one a try later!
