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4 answers

The answer to your question is very complex. You have to first understand how it generates lift and creates stability. Then you have to understand the controls (the cyclical and collective levers).

Here is the Wiki page for more info: http://en.wikipedia.org/wiki/Helicopter

2006-09-22 17:38:59 · answer #1 · answered by i_sivan 2 · 1 0

The rotor is shaped like an aircraft wing.

An aircraft wing generates lift when it moves forward through the air. The rotor blade generates lift in exactly the same way that an aircraft wing does, except that the engine rotates it forward. When the blade starts going backward a complicated linkage flips it so it generates lift going that way too.

As the engine turms, the helicopter tries to rotate the other way. The tail rotor stops it from doing that.

2006-09-22 20:16:15 · answer #2 · answered by Bob 7 · 0 0

The main rotor provides the lift and when angled the forward motion for the helicopter. The tail rotor is to offset the torque of the main rotor to prevent the helicopter from spinning in circles about the axis of the main rotor.

2006-09-22 17:39:47 · answer #3 · answered by jack w 6 · 1 0

Must use the devoted to the boundary conditions ,the torsional ,pressure and axially compressive loads ,as the eight sets of considered and the critical load , clamped shells subjected and more many aspects

2006-09-22 17:40:02 · answer #4 · answered by www. o 1 · 0 0

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