Characteristics Of A Helicopter

990 Words2 Pages

A helicopter is an aircraft that is heightened and propelled by one or more horizontal rotors, each rotor has two or more rotor blades. Helicopters are classified as rotary-wing aircraft to disperse them from fixed-wing aircraft because the helicopter derives its source of lift from the rotor blades rotating around a mast.
Using wings that generate the lift, forward aviation is what makes a helicopter fly. In powered airplanes, thrust from a jet engine is what moves the aircraft forward. The unique operating traits of the helicopter, its ability to take off and land vertically, to hover, and how it acts under poor airspeed conditions makes it helpful for tasks that were previously not possible with other aircraft. Helicopters are used for transportation, …show more content…

An airfoil is any surface producing more lift than drag when passing through the air at a suitable angle. Airfoils are most often associated with production of …show more content…

In the case of a helicopter, the object is the rotor blade (airfoil) and the fluid is the air. Lift is produced when a mass of air is deflected, and it always acts perpendicular to the resultant relative wind. Airfoil must have a positive AOA to generate positive lift. At a zero AOA, no lift is generated.
A quadcopter can move in 6 different axes. Drag: a rearward, retarding force caused by disruption of air ow by the wing, rotor, fuselage, and other protruding objects. Drag opposes thrust and acts rearward parallel to the relative wind. Weight: the combined load of the aircraft itself, the crew, the fuel, and the cargo or baggage. Weight pulls the aircraft downward because of the force of gravity. It opposes lift and acts vertically downward through the aircraft’s center of gravity (CG). Lift: opposes the downward force of weight, is produced by the dynamic effect of the air acting on the airfoil, and acts perpendicular to the flightpath through the center of lift. Thrust: generated by the rotation of the main rotor system. In a helicopter, thrust can be forward, rearward, sideward, or vertical. The resultant lift and thrust determines the direction of movement of the helicopter." Quadrotors work using a symmetrical design with the rotors located in each of the four corners. The rotors are fixed in their pitch with two of the rotors move clockwise

More about Characteristics Of A Helicopter

Open Document