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There is significantly more work that I have done on this problem since my last post.
From the frame of reference of an observer traveling down the ramp with the velocity of the center of mass of the fluid, the equations in the reference that I gave in a previous post can be expressed in terms of the angular velocity ##\omega## of the fluid by $$\frac{\partial \omega}{\partial t}=\nu\left(\frac{\partial ^2 \omega}{\partial r^2}+\frac{3}{r}\frac{\partial \omega}{\partial r}\right)\tag{1}$$where ##\nu## is the kinematic viscosity of the fluid ##\mu/\rho##. In addition, the shear stress exerted by the fluid on the wall of the can ##\tau_W## is given by $$\tau_W=\mu R\left(\frac{\partial \omega}{\partial r}\right)_{r=R}\tag{2}$$where ##\mu## is the dynamic viscosity of the fluid.
The overall force balance on the fluid-filled can (neglecting the mass and rotational inertia of the thin cylindrical shell) is given by $$\rho \pi R^2 L\frac{dv}{dt}=\rho\pi R^2L g\sin{\alpha}-F\tag{3}$$where F is the frictional force exerted by the ramp on the can surface. The frictional force F is related to the wall shear stress of the fluid on the inner radius of the can is given by $$F=2\pi RL\tau_W\tag{4}$$ (This equation assumes that the viscous drag exerted by the fluid on the lid and base of the can is negligible, or, equivalently, that the length to diameter ratio of the can is very large; note that, this is not really the case for the actual can, but, for now we will neglect the variation in angular velocity of the fluid with axial position within the can).
If we combine Eqns. 2-4, we obtain $$\rho \pi R^2 L\frac{dv}{dt}=\rho\pi R^2L g\sin{\alpha}-2\pi R^2 L\ \mu \left(\frac{\partial \omega}{\partial r}\right)_{r=R}\tag{5}$$or, equivalently,$$\frac{dv}{dt}=g\sin{\alpha}-2\nu\left(\frac{\partial \omega}{\partial r}\right)_{r=R}\tag{6}$$Kinematically, the velocity of the center of mass v is related to the rotation rate of the can surface ##\Omega=\omega(t,R)## by ##v=\Omega R##. Combining this with Eqn. 6 gives: $$\frac{d\Omega}{dt}=\frac{g\sin{\alpha}}{R}-2\frac{\nu}{R}\left(\frac{\partial \omega}{\partial r}\right)_{r=R}\tag{7}$$
Questions so far? After these are addressed, I will proceed further by reducing these equations to dimensionless form.
From the frame of reference of an observer traveling down the ramp with the velocity of the center of mass of the fluid, the equations in the reference that I gave in a previous post can be expressed in terms of the angular velocity ##\omega## of the fluid by $$\frac{\partial \omega}{\partial t}=\nu\left(\frac{\partial ^2 \omega}{\partial r^2}+\frac{3}{r}\frac{\partial \omega}{\partial r}\right)\tag{1}$$where ##\nu## is the kinematic viscosity of the fluid ##\mu/\rho##. In addition, the shear stress exerted by the fluid on the wall of the can ##\tau_W## is given by $$\tau_W=\mu R\left(\frac{\partial \omega}{\partial r}\right)_{r=R}\tag{2}$$where ##\mu## is the dynamic viscosity of the fluid.
The overall force balance on the fluid-filled can (neglecting the mass and rotational inertia of the thin cylindrical shell) is given by $$\rho \pi R^2 L\frac{dv}{dt}=\rho\pi R^2L g\sin{\alpha}-F\tag{3}$$where F is the frictional force exerted by the ramp on the can surface. The frictional force F is related to the wall shear stress of the fluid on the inner radius of the can is given by $$F=2\pi RL\tau_W\tag{4}$$ (This equation assumes that the viscous drag exerted by the fluid on the lid and base of the can is negligible, or, equivalently, that the length to diameter ratio of the can is very large; note that, this is not really the case for the actual can, but, for now we will neglect the variation in angular velocity of the fluid with axial position within the can).
If we combine Eqns. 2-4, we obtain $$\rho \pi R^2 L\frac{dv}{dt}=\rho\pi R^2L g\sin{\alpha}-2\pi R^2 L\ \mu \left(\frac{\partial \omega}{\partial r}\right)_{r=R}\tag{5}$$or, equivalently,$$\frac{dv}{dt}=g\sin{\alpha}-2\nu\left(\frac{\partial \omega}{\partial r}\right)_{r=R}\tag{6}$$Kinematically, the velocity of the center of mass v is related to the rotation rate of the can surface ##\Omega=\omega(t,R)## by ##v=\Omega R##. Combining this with Eqn. 6 gives: $$\frac{d\Omega}{dt}=\frac{g\sin{\alpha}}{R}-2\frac{\nu}{R}\left(\frac{\partial \omega}{\partial r}\right)_{r=R}\tag{7}$$
Questions so far? After these are addressed, I will proceed further by reducing these equations to dimensionless form.
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