/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 24 Two immiscible fluids are contai... [FREE SOLUTION] | 91Ó°ÊÓ

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Two immiscible fluids are contained between infinite parallel plates. The plates are separated by distance \(2 h\), and the two fluid layers are of equal thickness \(h=5 \mathrm{mm}\). The dynamic viscosity of the upper fluid is four times that of the lower fluid, which is \(\mu_{10 \text { wer }}=0.1 \mathrm{N} \cdot \mathrm{s} / \mathrm{m}^{2}\). If the plates are stationary and the applied pressure gradient is \(-50 \mathrm{kPa} / \mathrm{m}\) find the velocity at the interface. What is the maximum velocity of the flow? Plot the velocity distribution.

Short Answer

Expert verified
The velocity at the interface is \(0.05 m/s\), and the maximum velocity is also \(0.05 m/s\). The velocity distribution is represented by two overlapping parabolas showing that the velocity is \(0\) at the plates and maximum at the interface.

Step by step solution

01

Determine the velocity at the interface of the two fluids

By using the Navier-Stokes equation and considering the balance of forces in the direction of flow, you can write the equation as \( dp/dx = \mu * d^2u/dy^2 \), where \( p \) is the pressure, \( x \) is the distance along the flow, \( \mu \) is the dynamic viscosity and \( u \) is the velocity. By integrating twice and solving for constants using the boundary conditions that velocity \( u = 0 \) at \( y = 0 \) and \( y = h \), the velocity profile can be obtained. For the bottom layer with viscosity \( \mu_{1} \), \( u_{1}(y) = -dp/dx * (y^2/2\mu_{1} - h * y/\mu_{1} ) \). Similarly for the upper layer with viscosity \( \mu_{2} = 4\mu_{1} \), \( u_{2}(y) = -dp/dx * (y^2/2\mu_{2} - 2h * y/\mu_{2} + 3h^2/2\mu_{2} ) \). Substituting the given values of \( h = 0.005m \), \( \mu_{1} = 0.1Ns/m^2 \) and \( dp/dx = -50000Pa/m \) will give \( u_{1}(h) = u_{2}(h) = u_{interface} \).
02

Find the maximum velocity of the flow

To find the maximum velocity, the derivative of the velocity equation should be equated to zero and solved for y. By differentiating the velocity profile for each fluid layer and setting it to zero, \( du_{1}/dy = -dp/dx * (y - h) = 0 \) yields the maximum velocity \( u_{1max} = -dp/dx * h^2 / 2\mu_{1} \) occurs at \( y = h \). And \( du_{2}/dy = -dp/dx * (y - 2h) = 0 \) yields the maximum velocity \( u_{2max} = -dp/dx * h^2 / 2\mu_{2} \) occurs at \( y = 2h \).
03

Plot the velocity distribution

You plot the velocity profiles \( u_{1}(y) \) and \( u_{2}(y) \) with y ranging from 0 to 2h. The velocity should be zero at the plates and maximum at the interface, representing a parabolic profile.

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