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I've been looking at helicopter design recently, particularly UK military helicopters. I've noticed that most tail rotors are parallel/flush with the tail of the helicopter in most designs. When looking at the UH-60, I noticed that the tail rotor is diagonal WRT the tail (see image below).

My questions are:

  • Why is this?
  • Does this impact it's the ability to counter torque?
  • Does the rear rotor for the UH-60 have a component of lift?

enter image description here

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