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You're somewhat correct, but, in this case, the boundary layer thickness is the penetration depth of the velocity profile from a value of V at the rotating inner surface of the can to a value of zero in the bulk of the fluid away from the surface. Increasing the boundary layer thickness is the same as decreasing the velocity gradient in the fluid near the surface, which results in reduced drag on the surface as time progresses.mostafaelsan2005 said:So far I understood the question posed to solve the problem of viscous flow near a wall suddenly set in motion and I understand the working out generally but conceptually I do not understand the idea of 'boundary wall thickness'. After some research on it, I understand that it is 'the distance from this surface to the point where the velocity is 99% free-stream' and it depends on structural geometry which in this case is a cylinder and that increasing the boundary layer thickness increases the drag force experienced by the liquid in the can as an object moves. Is this a correct understanding up to now? Also, apologies for the late responses have been busy with interviews this week.
In Eqn. 1 of post #34, the velocity V is the tangential velocity of the inner surface of the can as reckoned by an observer who is traveling down the incline at the velocity of the center of mass of the can. As written, the equation assumes that the can rotation starts from rest and then stays constant for all subsequent time. But, in our system, the rotation rate of the can is not constant, but is changing as time progresses. The next issue to be addressed is how this equation can be modified to take this varying velocity history into consideration. Any ideas?