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The kinematic viscosity of a fluid is the ratio of viscosity to density, \(\nu=\mu / \rho .\) What is the only possible dimensionless group combining \(\nu\) with velocity \(V\) and length \(L ?\) What is the name of this grouping? (More information on this will be given in Chap. 5.)

Short Answer

Expert verified
The dimensionless group is the Reynolds number \(Re = \frac{VL}{\nu}\).

Step by step solution

01

Understand the problem

We need to find a dimensionless group involving the kinematic viscosity \(u\), velocity \(V\), and length \(L\). A dimensionless group means a combination of these variables that has no units.
02

Recall relevant non-dimensional numbers

The problem hints at a dimensionless group that involves \(u\), \(V\), and \(L\). One such well-known dimensionless number is the Reynolds number, which is a key concept in fluid dynamics.
03

Define the Reynolds number

The Reynolds number \(Re\) is defined as \(Re = \frac{VL}{u}\), where \(V\) is the velocity, \(L\) is the characteristic length, and \(u\) is the kinematic viscosity. This combination results in a dimensionless number.
04

Verify units are dimensionless

Ensure the units are consistent: \(u\) has units of \(m^2/s\), \(V\) has units of \(m/s\), and \(L\) has units of \(m\). Plugging these into \(Re = \frac{VL}{u}\) gives \(\frac{(m/s) \cdot m}{m^2/s} = \frac{m^2/s}{m^2/s} = 1\), confirming \(Re\) is dimensionless.

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Key Concepts

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

Kinematic Viscosity
Kinematic viscosity is an intrinsic property of fluids, playing a critical role in fluid dynamics. It defines the fluid's resistance to flow under the influence of gravity. Quantified as the ratio of dynamic viscosity, denoted by \( \mu \), to density \( \rho \), kinematic viscosity is expressed as:\[ u = \frac{\mu}{\rho} \]Measured in \( \text{m}^2/\text{s} \), kinematic viscosity reflects how fast molecules within a fluid can move relative to each other. Key features include:- **Dynamic Viscosity \( \mu \)**: Represents the internal friction within the fluid, measured in \( \text{Pa} \cdot \text{s} \).- **Density \( \rho \)**: Reflects the fluid's mass per unit volume, typically in \( \text{kg/m}^3 \).Understanding kinematic viscosity helps us comprehend and predict how different fluids behave. It is especially vital in scenarios like oil pipeline transport, where the ease of flow is crucial.
Thus, a higher kinematic viscosity signals a thicker fluid that moves more sluggishly, whereas a lower value indicates a more easily flowing fluid.
Dimensionless Groups in Fluid Mechanics
Dimensionless groups are pivotal in fluid mechanics, offering insight and clarity in fluid behavior comparisons across different scales and conditions. These groups, such as the Reynolds number, help by providing standardized benchmarks.The Reynolds number, in particular, is a dimensionless group involving velocity \( V \), length \( L \), and kinematic viscosity \( u \). It is quantified through:\[ Re = \frac{VL}{u} \]This calculation results in a pure number without any units, facilitating meaningful comparison across different fluids and geometries.
Such dimensionless numbers are important because:- They simplify complex fluid flow problems.- They help in the modeling of physical phenomena on different scales, assisting in connecting laboratory experiments to real-world applications.- They also aid in identifying flow regimes, such as distinguishing between laminar and turbulent flows. This simplification enables engineers and scientists to predict fluid behavior more easily, enhancing efficiency in design and analysis.
Fluid Dynamics Concepts
Fluid dynamics is a dynamic field focusing on the behavior of fluids in motion. This branch of physics examines how fluids interact with forces and encompasses fundamental principles that govern fluid motion. Core concepts include: - **Continuity Equation**: Ensures mass conservation in fluid flow, stating that the product of cross-sectional area and velocity must remain constant along a streamline. - **Bernoulli's Principle**: Explains how pressure varies with fluid flow speed, showing that an increase in a fluid's speed occurs simultaneously with a decrease in pressure or potential energy. - **Navier-Stokes Equations**: Provide a comprehensive description of how the velocity field of a fluid evolves over time, accounting for viscosity, pressure, and external forces. These principles apply to diverse applications, from designing efficient transportation systems to optimizing industrial processes.
By grasping fluid dynamics concepts, we can solve complex problems ranging from weather patterns to aerodynamics, making it an indispensable field in the modern scientific landscape.

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Most popular questions from this chapter

Algebraic equations such as Bernoulli's relation, Eq. (1) of Ex. \(1.3,\) are dimensionally consistent, but what about differential equations? Consider, for example, the boundary-layer \(x\) -momentum equation, first derived by Ludwig Prandtl in 1904 : $$\rho u \frac{\partial u}{\partial x}+\rho v \frac{\partial u}{\partial y}=-\frac{\partial p}{\partial x}+\rho g_{x}+\frac{\partial \tau}{\partial y}$$ where \(\tau\) is the boundary-layer shear stress and \(g_{x}\) is the component of gravity in the \(x\) direction. Is this equation dimensionally consistent? Can you draw a general conclusion?

The laminar-pipe-flow example of Prob. 1.12 can be used to design a capillary viscometer [27]. If \(Q\) is the volume flow rate, \(L\) is the pipe length, and \(\Delta p\) is the pressure drop from entrance to exit, the theory of Chap. 6 yields a formula for viscosity: $$\mu=\frac{\pi r_{0}^{4} \Delta p}{8 L Q}$$ Pipe end effects are neglected [27]. Suppose our capillary has \(r_{0}=2 \mathrm{mm}\) and \(L=25 \mathrm{cm} .\) The following flow rate and pressure drop data are obtained for a certain fluid: $$\begin{array}{l|l|l|l|l|l} Q, \mathrm{m}^{3} / \mathrm{h} & 0.36 & 0.72 & 1.08 & 1.44 & 1.80 \\ \hline \Delta p, \mathrm{kPa} & 159 & 318 & 477 & 1274 & 1851\end{array}$$ What is the viscosity of the fluid? Note: Only the first three points give the proper viscosity. What is peculiar about the last two points, which were measured accurately?

Experiment with a faucet (kitchen or otherwise) to determine typical flow rates \(Q\) in \(\mathrm{m}^{3} / \mathrm{h}\), perhaps timing the discharge of a known volume. Try to achieve an exit jet condition which is \((a)\) smooth and round and \((b)\) disorderly and fluctuating. Measure the supply-pipe diameter (look under the sink). For both cases, calculate the average flow velocity, \(V_{\mathrm{avg}}=\) \(Q / A_{\text {cross-section }}\) and the dimensionless Reynolds number of the flow, \(\operatorname{Re}=\rho V_{\text {avg }} D / \mu .\) Comment on your results.

For low-speed (laminar) steady flow through a circular pipe, as shown in Fig. P1.12, the velocity \(u\) varies with radius and takes the form $$u=B \frac{\Delta p}{\mu}\left(r_{0}^{2}-r^{2}\right)$$ where \(\mu\) is the fluid viscosity and \(\Delta p\) is the pressure drop from entrance to exit. What are the dimensions of the constant \(B ?\)

Air at 1 atm and \(20^{\circ} \mathrm{C}\) has an internal energy of approximately 2.1 E5 J/kg. If this air moves at \(150 \mathrm{m} / \mathrm{s}\) at an altitude \(z=8 \mathrm{m},\) what is its total energy, in \(\mathrm{J} / \mathrm{kg},\) relative to the datum \(z=0 ?\) Are any energy contributions negligible?

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