A helicopter flies off, its propellers rotating. Why doesn't the body

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Discussion Overview

The discussion centers on the mechanics of helicopter flight, specifically addressing why the body of a helicopter does not rotate in the opposite direction of its main rotor's rotation. The scope includes technical explanations of helicopter design and anti-torque systems.

Discussion Character

  • Technical explanation, Conceptual clarification, Debate/contested

Main Points Raised

  • Some participants propose that a tail rotor generates a sideways force to counteract the torque produced by the main rotor, preventing the helicopter body from rotating in the opposite direction.
  • Others explain that the torque from the main rotor must be balanced, or else the helicopter body will rotate in the opposite direction.
  • A participant mentions various methods developed to achieve torque balance, including secondary rotors and contra-rotating lift rotors.
  • Another participant introduces the NOTAR system, which replaces the tail rotor with a fan system to create thrust that counteracts the torque effect of the main rotor.

Areas of Agreement / Disagreement

Participants generally agree on the need for a counteracting force to balance the torque from the main rotor, but multiple competing views on the methods to achieve this remain, including traditional tail rotors and alternative systems like NOTAR.

Contextual Notes

Some claims depend on specific design choices and may not address all helicopter configurations. The discussion does not resolve the effectiveness or applicability of the various systems mentioned.

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A helicopter flies off, its propellers rotating. Why doesn't the body of the helicopter rotate in the opposite direction?
 
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A tail rotor is used to generate a sideways force that results in an opposing torque. The side force causes the helicopter to drift to the side a bit unless the helicopter leaned a small amount.
 


Yes you are correct in observing that the torque driving the main rotor has to be balanced or the body of the copter will rotate the other way.

If you ever visit the Helicopter Museum at Weston Super Mare in England (recommended) you will see examples of all the schemes developed to achieve this.

The principle method is a secondary rotor, revolving about an axis perpendicular to the main rotor, driving the tail the other way.
Other important methods, used particularly in very large helicopters, are to have a second lift rotor, rotating in such a direction as to produce a balancing torque on the body. The second lift rotor is contra-rotating and either mounted vertically above the first or the two rotors are mounted at opposing ends of the body.
 
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There is also the NOTAR system, which is pretty cool. A brief quote from Wiki:

NOTAR is the name of a helicopter anti-torque system which replaces the use of a tail rotor on a helicopter. Developed by McDonnell Douglas Helicopter Systems, the name is an acronym derived from the phrase NO TAil Rotor. The system uses a fan inside the tailboom to build a high volume of low-pressure air, which exits through two slots and creates a boundary layer flow of air along the tailboom utilizing the Coandă effect. The boundary layer changes the direction of airflow around the tailboom, creating thrust opposite the motion imparted to the fuselage by the torque effect of the main rotor. Directional yaw control is gained through a vented, rotating drum at the end of the tailboom, called the direct jet thruster. Advocates of NOTAR believe the system offers quieter and safer operation.[1]
 

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