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The velocity profile in fully developed laminar flow in a circular pipe, in \(\mathrm{m} / \mathrm{s}\), is given by \(u(r)=6\left(1-100 r^{2}\right)\) where \(r\) is the radial distance from the centerline of the pipe in \(\mathrm{m}\). Determine \((a)\) the radius of the pipe, \((b)\) the mean velocity through the pipe, and \((c)\) the maximum velocity in the pipe.

Short Answer

Expert verified
Answer: The radius of the pipe is \(0.1\thinspace\text{m}\), the mean velocity through the pipe is \(5.98\thinspace\text{m/s}\), and the maximum velocity in the pipe is \(6\thinspace\text{m/s}\).

Step by step solution

01

Find the radius of the pipe

To find the radius of the pipe, we have to find the point where the velocity profile becomes zero (at the pipe wall). So, we will solve the equation \(u(r) = 0\) for \(r\). \(u(r)=6\left(1-100 r^{2}\right) = 0\) Now, solve for \(r\): \(1-100r^2 = 0\) \(r^2 = \frac{1}{100}\) \(r=\sqrt{\frac{1}{100}}\) \(r=0.1 \thinspace\text{m}\) So, the radius of the pipe is \(0.1 \thinspace\text{m}\).
02

Find the mean velocity through the pipe

To find the mean velocity, we will integrate the velocity profile over the pipe's cross-sectional area and divide by the area. The cross-sectional area of a circular pipe is given by \(A = \pi R^2\), where \(R\) is the radius of the pipe. The mean velocity, \(U\), is given by: \(U = \frac{1}{A} \int_{0}^{R} u(r) \cdot 2\pi r \thinspace dr\) Using the given velocity profile, \(u(r) = 6(1 - 100r^{2})\), and radius \(R = 0.1\thinspace\text{m}\), we get: \(U = \frac{1}{\pi (0.1)^2} \int_{0}^{0.1} 6(1-100r^2) \cdot 2\pi r \thinspace dr\) \(U = \frac{1}{0.01\pi} \int_{0}^{0.1} 12\pi r(1-100r^2) \thinspace dr\) Now, integrate with respect to r: \(U = \frac{1}{0.01\pi} \left[ 6\pi r^2 - 2\pi r^4\right]_0^{0.1}\) \(U = \frac{1}{0.01\pi}\left[ 6\pi (0.1)^2 - 2\pi (0.1)^4\right]\) \(U = \frac{1}{0.01\pi} \left[0.06\pi - 0.0002\pi \right]\) \(U = 6-0.02 \thinspace\text{m/s}\) Thus, the mean velocity through the pipe is \(5.98\thinspace\text{m/s}\).
03

Find the maximum velocity in the pipe

The maximum velocity is at the centerline of the pipe, where the derivative of the velocity profile is zero. To find the maximum velocity, we need to calculate the derivative of the velocity profile with respect to \(r\) and find its value at \(r = 0\). Take the derivative of \(u(r) = 6\left(1-100 r^{2}\right)\) with respect to \(r\): \(\frac{du}{dr} = 6 \cdot (-200r)\) Now, evaluate the velocity profile at \(r = 0\): \(u_\text{max} = u(0) = 6\left(1-100(0)^2\right)\) \(u_\text{max} = 6 \thinspace\text{m/s}\) So, the maximum velocity in the pipe is \(6 \thinspace\text{m/s}\).

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Velocity Profile
In fluid dynamics, especially when analyzing flow through pipes, the velocity profile is crucial. For laminar flow, it indicates how the velocity of the fluid varies across the pipe's diameter. This profile provides vital clues about how fast or slow the fluid particles move at various radial positions within the pipe. In the context of our exercise, the velocity profile is given by the formula:\[u(r) = 6(1 - 100r^2)\]- **Formula Explanation**: - **6** indicates that at the center (where r is 0), the velocity is initially 6 m/s. - **100r^2** shows the parabolic nature of the velocity decrease from the center towards the pipe wall.As one moves away from the center, the velocities drop quadratically because of the squared r term. Understanding this parabolic profile helps in figuring out both the mean and maximum velocities within the pipe.
Circular Pipe
Circular pipes are a common medium for fluid transport due to their symmetry, which leads to uniform flow distribution. The flow characteristics within these pipes—especially for laminar flow, as in our example—are predictable and consistent. The circular geometry simplifies the mathematics involved in calculating the velocity profile as it allows for symmetrical flow about the central axis.To determine the pipe's radius, one finds the boundary at which the velocity becomes zero. For the given velocity equation, this is solved by setting \(u(r) = 0\). Through these calculations, we identify that the radius of the pipe is 0.1 m. Understanding this property is essential, as it directly influences calculations for mean and maximum velocities.
Mean Velocity
Mean velocity in a pipe is defined as the average velocity of the fluid particles across the entire cross-sectional area of the pipe. While the velocity profile gives instant velocities at specific points, the mean velocity provides a macroscopic view, representing the overall flow within the pipe.To find mean velocity:- **Integration Approach**: The integral of the velocity profile across the entire cross-section (from the center to the wall) provides total volume flow.- Divide by the area to obtain the mean velocity.In our example, the mean velocity was calculated through integration of:\[U = \frac{1}{\pi (0.1)^2} \int_{0}^{0.1} 6(1-100r^2) \cdot 2\pi r \thinspace dr\]After solving, the mean flow velocity through the pipe is found to be 5.98 m/s. This mean velocity is always less than the maximum velocity, as it represents the balance of lower and higher velocities across the profile.
Maximum Velocity
In the context of a parabolic velocity profile like ours, maximum velocity is found right at the center of the pipe where the fluid's radial distance is zero. This stems from the lack of frictional resistance from the walls, allowing the fluid at the center to move at the highest speed possible.- **Derivative Insight**: By taking the derivative of the velocity profile, one can confirm that the flow at the center is indeed the maximum point. Setting derivatives equal to zero would give the radial point (r=0) needing checking.- **Velocity at Center (r=0):**The velocity profile equation evaluated at r=0 gives us:\[u_{max} = u(0) = 6(1 - 100(0)^2)\]Resulting in a maximum velocity of 6 m/s. This is always greater than the mean velocity, as the flow slows towards the sides due to friction with the pipe walls.

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Most popular questions from this chapter

Air is flowing through a smooth thin-walled 4-indiameter copper tube that is submerged in water. The water maintains a constant temperature of \(60^{\circ} \mathrm{F}\) and a convection heat transfer coefficient of \(176 \mathrm{Btu} / \mathrm{h}-\mathrm{ft}^{2} \cdot \mathrm{R}\). If air (1 atm) enters the copper tube at a mean temperature of \(90^{\circ} \mathrm{F}\) with an average velocity of \(8 \mathrm{ft} / \mathrm{s}\), determine the necessary copper tube length so that the outlet mean temperature of the air is \(70^{\circ} \mathrm{F}\).

How is the hydrodynamic entry length defined for flow in a tube? Is the entry length longer in laminar or turbulent flow?

Consider laminar forced convection in a circular tube. Will the heat flux be higher near the inlet of the tube or near the exit? Why?

What is the physical significance of the number of transfer units NTU \(=h A_{s} / \dot{m} c_{p}\) ? What do small and large NTU values tell about a heat transfer system?

Cooling water available at \(10^{\circ} \mathrm{C}\) is used to condense steam at \(30^{\circ} \mathrm{C}\) in the condenser of a power plant at a rate of \(0.15 \mathrm{~kg} / \mathrm{s}\) by circulating the cooling water through a bank of 5 -m-long \(1.2-\mathrm{cm}\)-internal-diameter thin copper tubes. Water enters the tubes at a mean velocity of \(4 \mathrm{~m} / \mathrm{s}\) and leaves at a temperature of \(24^{\circ} \mathrm{C}\). The tubes are nearly isothermal at \(30^{\circ} \mathrm{C}\). Determine the average heat transfer coefficient between the water, the tubes, and the number of tubes needed to achieve the indicated heat transfer rate in the condenser.

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