There seem to be a few arguments:
[ul][li]JimB: The centrifugal force of going around the curve is the same in the case of squirting or sucking, so it spins the same in either case.[/li][li]hansel: The act of water being sucked in will suck the tube along, in exactly the time-reversed way that squirting makes it spin the other way. It turns out this is correct, though not because of the suction acting like reverse thrust theory.[/li][li]Scylla: It doesn’t go anywhere because the water going into the tube is coming from all directions and is not directed like it is in the case of a squirt.[/ul][/li]
First, lets cover the ‘suction as a time-reversal of squirting’ option. This can’t be because fluid that is moving will willingly change directions when being sucked but not when being squirted. To see the difference, hold your hair dryer up and see how far away you can be and still feel the air blast. Now, hold your vacuum cleaner and see how far away you can feel the suction - it’s a much smaller distance. As Scylla said, the water does go in from all directions. Picture someone exhaling a bunch of cigarette smoke. It shoots out in a fairly straight line, then diffuses. Now imagine seeing that film in reverse - all the smoke shooting straight into the guys mouth like a piece of spaghetti. Not gonna happen. Simpler experiment: Blow out a candle. Now, light it again and try to ‘suck’ it out. (danger :Don’t do this if there is the remotest chance you could hurt yourself and sue me.)
So, the suction option doesn’t fly. What about the centrifugal force? The argument about the jet engine is intriguing, though it is worth noting in passing that it demonstrates that the suction of the engine is not what provides thrust, lending more credence to the above logic.
But what about the change in direction (centrifugal force) vs. reaction thrust (rocket-engine type propulsion)? Without doing any math, let me try to convince you it is the thrust that matters most. If it is the change in direction that is important, a jet engine with reversers deployed and running in reverse would work just as well to stop the plane as with the engine running normally.
Let’s just think about this. A jet engine running normally without the reversers achieves a lot of thrust without any direction changing of exhaust. Thus, the thrust must be important. If we now deploy the reversers and the thrust points in the other direction with 100% efficiency (not the case, but let’s just say) then the engine is working just as well to slow the plane.
But wait! We get the extra bonus of the change of direction of the thrust bouncing off the reversers! That must be ADDED to the engine’s thrust, giving a more efficient engine! So then, jet engines should be mounted backwards and fly with their reversers deployed to take advantage of this.
Nope, if Boeing could eke another 5% efficiency out of a jet engine they’d do it in a heartbeat. So, it must be the thrust that matters most, and since we can’t ‘suck’ thrust, the forces on the inverse sprinkler are going to be smaller.
The final answer is, yes, the change in direction is a component of the forces on the sprinkler (or the jet engine) but it is small compared to the thrust component, and it is exactly balanced by the much smaller suction-anti-thrust component.
In fact, if you have a very good experimental setup, you will get the thing to go in the suction direction, but only slowly. The only reason that an inverse sprinkler goes in the opposite direction of the normal sprinkler is the angular momentum change that Scylla describes above with his jerky water hose. After the flow becomes steady, the sprinkler stays spinning slowly, as opposed to spinning quickly when squirting. And, if you add any friction, the thing will just sit there.
Links:
[ul][li]Not terribly helpful: MIT’s Edgerton Center[/li][li]Much better: University of Maryland Physics[/li]Also good: http://www.wiskit.com/marilyn/sprinkler.html[/ul]