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

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A helicopter's body does not rotate in the opposite direction of its main rotor due to the use of a tail rotor, which generates a sideways force to counteract the torque. If this torque is unbalanced, the helicopter would rotate in the opposite direction. Alternative methods for torque balance include secondary rotors and contra-rotating lift rotors, which can be positioned vertically or at opposing ends of the helicopter. The NOTAR system eliminates the tail rotor by using a fan to create airflow along the tailboom, providing thrust to counteract torque. These systems enhance stability, control, and safety in helicopter operation.
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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]
 
I built a device designed to brake angular velocity which seems to work based on below, i used a flexible shaft that could bow up and down so i could visually see what was happening for the prototypes. If you spin two wheels in opposite directions each with a magnitude of angular momentum L on a rigid shaft (equal magnitude opposite directions), then rotate the shaft at 90 degrees to the momentum vectors at constant angular velocity omega, then the resulting torques oppose each other...

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