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The velocity profile, \(v(r),\) for turbulent flow in smooth pipes is sometimes estimated by the seventh-root law, originally proposed by Blasius (1913) as $$ v(r)=V_{0}\left(1-\frac{r}{R}\right)^{\frac{1}{7}} $$ where \(V_{0}\) is the centerline velocity and \(R\) is the radius of the pipe. Estimate the energy and momentum correction factors corresponding to the seventh-root law.

Short Answer

Expert verified
The energy correction factor \( \alpha \) is approximately 1.047 and the momentum correction factor \( \beta \) is approximately 1.017.

Step by step solution

01

Understand Energy and Momentum Correction Factor Formulas

The energy correction factor, \( \alpha \), and momentum correction factor, \( \beta \), are determined by integrating the velocity profile across the pipe's cross-section.- The energy correction factor, \( \alpha \), is calculated as: \[ \alpha = \frac{\int_{0}^{R} v(r)^3 \, 2 \pi r \, dr}{V^3 A} \] where \( V \) is the average velocity and \( A = \pi R^2 \) is the cross-sectional area.- The momentum correction factor, \( \beta \), is calculated as: \[ \beta = \frac{\int_{0}^{R} v(r)^2 \, 2 \pi r \, dr}{V^2 A} \]These equations require the evaluation of integrals over the velocity profile \( v(r) \).
02

Express Average Velocity in Terms of Centerline Velocity

The average velocity \( V \) is obtained by integrating the velocity profile across the pipe's cross-section and dividing by the area:\[ V = \frac{1}{A} \int_{0}^{R} v(r) \, 2 \pi r \, dr = \frac{2 \pi}{\pi R^2} \int_{0}^{R} V_{0}\left(1-\frac{r}{R}\right)^{\frac{1}{7}} r \, dr \]This simplifies to:\[ V = \frac{2 V_{0}}{R^2} \int_{0}^{R} \left(1-\frac{r}{R}\right)^{\frac{1}{7}} r \, dr \]
03

Evaluate the Average Velocity Integral

Substitute \( x = \frac{r}{R} \), so \( dr = R \, dx \). Then the integral becomes:\[ V = \frac{2 V_{0}}{R} \int_{0}^{1} (1-x)^{\frac{1}{7}} x \, dx \]Solving this integral using the integral of the form \( \int x^m (1-x)^n \, dx \) requires integration techniques or numerical methods. This yields:\[ V = \frac{14}{15} V_0 \]
04

Calculate Energy Correction Factor

Substitute the seventh-root law into the energy correction factor formula:\[ \alpha = \frac{2 \pi}{V^3 \pi R^2} \int_{0}^{R} \left(V_0 \left(1-\frac{r}{R}\right)^{\frac{1}{7}}\right)^3 r \, dr \]Using previously derived \( V = \frac{14}{15} V_0 \), substitute and simplify yields:\[ \int_{0}^{1} (1-x)^{\frac{3}{7}} x \, dx \]The integration can be done yielding:\[ \alpha \approx 1.047 \]
05

Calculate Momentum Correction Factor

Substitute the seventh-root law into the momentum correction factor formula:\[ \beta = \frac{2 \pi}{V^2 \pi R^2} \int_{0}^{R} \left(V_0 \left(1-\frac{r}{R}\right)^{\frac{1}{7}}\right)^2 r \, dr \]Simplify using \( V = \frac{14}{15} V_0 \), and solve:\[ \int_{0}^{1} (1-x)^{\frac{2}{7}} x \, dx \]The integration gives:\[ \beta \approx 1.017 \]
06

Conclusion: Correction Factors for Seventh-root Law

The energy correction factor \( \alpha \) is approximately 1.047, and the momentum correction factor \( \beta \) is approximately 1.017. Both indicate that the turbulent velocity profile has minor deviations from an ideal profile due to inertia effects.

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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, understanding the velocity profile is crucial for predicting flow behavior within pipes or channels. For turbulent flow, which is characterized by chaotic changes in pressure and flow velocity, the velocity profile describes how the velocity of the fluid varies across the pipe's cross-section.
The seventh-root law, proposed by Blasius, is a common model used to estimate this profile in smooth pipes. It expresses the velocity profile as follows: \[ v(r) = V_0 \left( 1 - \frac{r}{R} \right)^{\frac{1}{7}} \] where \( V_0 \) is the centreline velocity (at the centre of the pipe where \( r = 0 \)), and \( R \) is the pipe's radius. This formula helps in predicting how velocity decreases from the maximum at the centre to zero at the pipe wall.
Energy Correction Factor
The energy correction factor, denoted as \( \alpha \), is essential for evaluating fluid flow in pipes since it accounts for the distribution of velocity across the cross-section. In real-world turbulent flow conditions, velocity isn't uniform, and this factor helps correct the calculated energy.
The formula for the energy correction factor is: \[ \alpha = \frac{\int_{0}^{R} v(r)^3 \, 2 \pi r \, dr}{V^3 A} \] where \( V \) is the average velocity and \( A \) is the pipe's cross-sectional area. This equation involves integrating the cube of the velocity profile over the cross-section.- Using \( v(r) = V_0 \left(1 - \frac{r}{R}\right)^{\frac{1}{7}} \), we integrate the velocity profile to find \( V \)- The intricate nature of this integral often requires numerical methods.
The result gives insight into how velocity variations affect energy losses in a turbulent system.
Momentum Correction Factor
The momentum correction factor, represented by \( \beta \), evaluates how the velocity distribution affects momentum flow through a cross-section of a pipe. Like the energy correction factor, \( \beta \) corrects predictions of fluid momentum that suppose uniform velocity. The formula for \( \beta \) is: \[ \beta = \frac{\int_{0}^{R} v(r)^2 \, 2 \pi r \, dr}{V^2 A} \] To calculate \( \beta \), substitute the velocity profile from Blasius's law, then perform the integration:- Similar to the energy correction factor, this involves integrating the square of the velocity profile. - This process accounts for the real fluid conditions that deviate from ideal assumptions, primarily arising from shear stress and eddies.
These corrections ensure that calculations involving fluid flow momentum are more accurate.
Integral Calculus
Integral calculus is essential in fluid dynamics for calculating various flow properties, like the average velocity, energy, and momentum corrections. It involves integrating functions over certain domains, particularly across pipe cross-sections in this context.Using integral calculus:- Integrates the velocity profile over the pipe's cross-section to quantify average velocity \( V \).- Essential for deriving formulas such as the correction factors, where velocity distributions are defined by complex expressions, like the seventh-root formula: \[ \int_{0}^{R} v(r) \, 2 \pi r \, dr \] Common techniques involve substitutions and change of variables, sometimes integrating through known forms like \( x^m (1-x)^n \).
This approach helps in resolving the velocity distributions into manageable figures indicative of the fluid's true behavior.
Blasius Profile
The Blasius profile is a classical solution describing velocity profiles in laminar and turbulent flow regimes within pipes. Its seventh-root law adaptation helps model turbulent flows in pipes and channels, offering a simplified but effective approximation of velocity distribution. This profile is significant because: - It approximates the way in which velocity drops from the peak at the centerline to the boundary. - By using the seventh-root formulation, it provides an empirical approach suitable for computations without relying on time-intensive computations of turbulent eddies. The impact of the Blasius profile is evident in its application for calculating correction factors and average velocities relevant to fluid mechanics. In practical use, it allows engineers and scientists to model and predict turbulent behavior efficiently, though real-world conditions may require adjustments based on additional factors like surface roughness or transition layers.

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Most popular questions from this chapter

Water flows at a rate of \(100 \mathrm{~L} / \mathrm{s}\) in a \(100-\mathrm{m}\) section of 200 -mm-diameter ductile iron pipeline, where the end of the pipeline has an elevation that is \(0.8 \mathrm{~m}\) higher than the beginning of the pipeline. Under the given flow condition, the pressure at the end of the pipeline is measured to be \(90 \mathrm{kPa}\) less than the pressure at the beginning of the pipeline. (a) Estimate the friction factor of the pipeline. (b) Assess the condition of the pipeline in terms of likely deterioration of the interior surface of the pipeline.

Water at \(20^{\circ} \mathrm{C}\) flows in a \(150-\mathrm{m}\) -long, 50 -mm- diameter ductile iron pipe at \(4 \mathrm{~m} / \mathrm{s}\). The thickness of the pipe wall is \(1.5 \mathrm{~mm},\) and the modulus of elasticity of ductile iron is \(1.655 \times 10^{5} \mathrm{MN} / \mathrm{m}^{2}\). What is the maximum water hammer pressure that can occur?

A 125 -mm-diameter duct admits air from a chamber in which the air temperature is \(80^{\circ} \mathrm{C}\) and the air pressure is \(101.3 \mathrm{kPa}\) (absolute). (a) Determine the minimum volume inflow rate required to ensure that the flow in the duct is turbulent. (b) At the limiting condition determined in part (a), what is the hydrodynamic entrance length required for fully developed flow in the duct?

Water at \(20^{\circ} \mathrm{C}\) flows through a 125 -mm-diameter steel pipe at a rate of \(10 \mathrm{~L} / \mathrm{s}\). The equivalent sand roughness of the pipe is estimated as \(0.3 \mathrm{~mm}\). (a) Estimate the friction factor of the flow. (b) Estimate the thickness of the viscous layer adjacent to the pipe surface. (c) Compare the thickness of the viscous layer to the sand roughness to estimate whether the flow is in the regime of smooth pipe, transition, or rough pipe.

A pump creates a water pressure of 1 MPa in the supply line to a 65 -mm- diameter, 300 -m-long hose with a roughness height of \(0.5 \mathrm{~mm}\). The end of the hose is at an elevation \(2.8 \mathrm{~m}\) higher than the beginning of the hose. The objective is to place a nozzle at the end of the hose that will create a jet of water that rises \(30 \mathrm{~m}\) into the air. If the local head loss coefficient of the nozzle is \(0.04,\) what nozzle diameter should be used? Assume water at \(20^{\circ} \mathrm{C}\).

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