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In a NOTAR helicopter the redirection of the main rotor downwash to counter-act torque is the classic application of the
Coanda effect
Movement of the helicopter around the____ axis is called roll.
Longitudinal
Movement of the helicopter around the axis produces a nose-up or nose-down attitude, or___
Lateral Axis, Pitch
Movement of the helicopter around the _____axis produces a change in direction to the right or left called _
Vertical, yaw
Circle one; (TRUE/FALSE ) The Upper Swash Plate rotates the same direction with the main rotor hub and the Lower Swash Plate rotates in the opposite direction to counteract torque.
False
An _____is simply molded, rubber-like material bonded to the appropriate part that allows proper movement.
Elastomeric bearing
The free-wheeling unit, that enables a helicopter to autorotate, comes in different forms, with the most popular being the
Sprag clutch
The type of Main Rotor Head where the blades are rigidly interconnected and pivot about a point slightly above their center is called ____
Semi rigid
Which of these stops accidents from tail rotor, strikes by eliminating the tail rotor all together
Notar
Which of these are used in coordination to regulate the airspeed?
Collective pitch control and cycle pitch control
The change of a helicopter from the hover to flying is called?
Transition
The torque effect is the tendency of the helicopter to rotate in the opposite direction the main rotor because of newton's?
The third law motion
Blades that can lead and lag individually during rotation are characteristic of which type of the tail rotor hub?
Fully articulated type
With a helicopter in a motionless hover the tail rotor wants the helicopter to drift in the direction which it is producing anti-torque thrust. This is called?
Translating tendency
To change the angle of attack of the blades, move the:
Cyclic control stick
A fully articulated rotor head gets its name because it is:
Jointed
Which of these tail rotor types is safer both on the ground and in flight because of a fan should?
Fenestron
Essay
Describe, in detail, the operation of the Collective Pitch Control and how it operates from the cockpit up to the main rotor.
Raising the collective pitch control increases the pitch of the main rotor.
Describe, in detail, the operation of the Cyclic Pitch Control and how it operates from the cockpit up to the main rotor.
Moving the cycle control stick changes the angle of attack of the blade
How and why is a helicopter able to autorotate (glide) to the ground.
The free-wheeling unit allows the engine to drive the rotors but bit the rotors to drive the engine.