I work at NASA. We had a big review meeting for a space brayton (turbine engine) concept. One manager-level engineer absolutely thought that the spinning rotor would apply a constant torque to the spacecraft that would have to be constantly counteracted. I tried and failed to explain conservation of angular momentum to him.
I studied physics and it always surprises me how many good engineers really don’t have a very good intuitive understanding of basic physics principles like conservation laws.
I’m just checking my intuition here. An accelerating or decelerating rotor would apply an angular force (first derivative), while a constant rotation would not?
I'm confused... you are right that it takes no additional torque to keep a frictionless rotor rotating at the same angular velocity, but in the real world there is friction and air resistance where you have to keep applying torque to keep something spinning at the same rate. and if you are applying torque to someone, then that thing is applying an equal and opposite torque back... is it not?
> if you are applying torque to someone, then that thing is applying an equal and opposite torque back
Yes, just like with a force.
> but in the real world there is friction and air resistance where you have to keep applying torque to keep something spinning at the same rate
Yes, but I think you are forgetting one thing: If the friction is between the rotor and the body, then this friction does not only act on the rotor, but also on the body. I.e. the friction creates a pair of torques which the engine can perfectly counteract with it's own pair of torques.
If the friction is between the rotor and the air, then yes, the spacecraft needs some kind of counteraction or it will start turning.
I suspect that the engineer in the GP's story might not remember the equations for angular acceleration, but has an intuitive sense that if a spinning something is in contact with a non-spinning something, you need a good reason for why some of the energy won't get transferred from the former to the latter.
Yes and no. The torque in helicopter is primarily a side effect of power being applied to the rotor. When a helicopter auto rotates (such as after an engine failure), the pilot has to remove anti torque forces with the pedals. This remains true even when you change pitch to slow your descent to the ground. So as long as no power is being applied, if you are in a free descent with a constant rotation on your rotor, then no, you will not need anti torque.
No, because the main router isn’t applying a pure downward thrust. It’s also moving air in the direction of rotation. A turbine has internal baffles and the ducting itself to direct the air in one direction (?)
I studied physics and it always surprises me how many good engineers really don’t have a very good intuitive understanding of basic physics principles like conservation laws.