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SIFT Army Aviation Information Exam Questions and Answers Already Passed Latest Update

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SIFT Army Aviation Information Exam Questions and Answers Already Passed Latest Update Four forces acting on a helicopter in flight. - Answers Lift, Thrust, Weight, Drag Induced Drag - Answers That part of the drag on an airfoil that arises from the development of lift. Parasite Drag - Answers Drag from components that don't create lift. (Wheels, Fuselage) The Venturi Effect - Answers The Venturi effect is the reduction in fluid pressure that results when a fluid flows through a constricted section (or choke) of a pipe. Cyclic Control - Answers Used to control direction/ tilt of aircraft. The Collective (Control) - Answers Left side of the pilot, moves up and down. Alters angle of attack of rotor blades Throttle - Answers Controls power produced by the engine Anti-torque pedals - Answers Control the yaw of the aircraft, where it is pointing Advancing blade - Answers Airfoil - Answers Either the rotor blades themselves or the horizontal stabilizers. Angle of Attack - Answers The angle between the chord line of an airfoil and the airfoil's direction of motion relative to the air. (Aerodynamic Angle) Angle of Incidence - Answers Angle between chord line of each blade and the rotor system's place of rotation. (Mechanical Angle) Autorotation - Answers Loss of engine power, angle down so that air keeps the rotors spinning. Freewheeling unit disconnects. Blade Span - Answers Length from top of blade to drive shaft. Chord/Chord Line - Answers Coning/ Coning Angle - Answers Coning angle is the difference between the line perpendicular to the mast and the blades in motion. Coriolis Effect - Answers A rotating body spins at the same speed unless acted upon by an external force. Dissymmetry of Lift - Answers The advancing blade experiences greater wind speed and as such produces more lift than the retreating side. The is counteracted by allowing blades to flap

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SIFT Army Aviation Information Exam Questions and Answers Already Passed Latest Update

Four forces acting on a helicopter in flight. - Answers Lift, Thrust, Weight, Drag

Induced Drag - Answers That part of the drag on an airfoil that arises from the development of lift.

Parasite Drag - Answers Drag from components that don't create lift. (Wheels, Fuselage)

The Venturi Effect - Answers The Venturi effect is the reduction in fluid pressure that results when a fluid
flows through a constricted section (or choke) of a pipe.

Cyclic Control - Answers Used to control direction/ tilt of aircraft.

The Collective (Control) - Answers Left side of the pilot, moves up and down. Alters angle of attack of
rotor blades

Throttle - Answers Controls power produced by the engine

Anti-torque pedals - Answers Control the yaw of the aircraft, where it is pointing

Advancing blade - Answers

Airfoil - Answers Either the rotor blades themselves or the horizontal stabilizers.

Angle of Attack - Answers The angle between the chord line of an airfoil and the airfoil's direction of
motion relative to the air. (Aerodynamic Angle)

Angle of Incidence - Answers Angle between chord line of each blade and the rotor system's place of
rotation. (Mechanical Angle)

Autorotation - Answers Loss of engine power, angle down so that air keeps the rotors spinning.
Freewheeling unit disconnects.

Blade Span - Answers Length from top of blade to drive shaft.

Chord/Chord Line - Answers

Coning/ Coning Angle - Answers Coning angle is the difference between the line perpendicular to the
mast and the blades in motion.

Coriolis Effect - Answers A rotating body spins at the same speed unless acted upon by an external force.

Dissymmetry of Lift - Answers The advancing blade experiences greater wind speed and as such
produces more lift than the retreating side. The is counteracted by allowing blades to flap up and down.

Driven Region - Answers Has the effect of slowing the rotor's spin.

Driving Region - Answers Supply's thrust.

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