A very small needle valve is used to control the flow of air in a \(\frac{1}{8}-\) in. air line. The valve has a pressure drop of 4.0 psi at a flow rate of \(0.005 \mathrm{ft}^{3} / \mathrm{s}\) of \(60^{\circ} \mathrm{F}\) air. Tests are performed on a large, geometrically similar valve and the results are used to predict the performance of the smaller valve. How many times larger can the model valve be if \(60^{\circ} \mathrm{F}\) water is used in the test and the water flow rate is limited to 7.0 gal/min?

Short Answer

Expert verified
The measure of how much larger the model valve can be is obtained using above steps. Remember to calculate the value of \(Q_{water}\) in Step 1 before substituting into the equation. Increase in size is still relative to the original size.

Step by step solution

01

Convert given flow rate of water from gal/min to ft³/s.

First, let's convert the flow rate of water from gallons per minute to cubic feet per second. Water flow rate = 7.0 gal/min The conversion factor from gallons to cubic feet is 0.133681 and from minutes to seconds is 1/60. So, \(Q_{water} = 7.0 \times 0.133681 \times \frac{1}{60}~\mathrm{ft}^{3}/\mathrm{s}\)
02

Apply the Reynolds number principle

As the valves are geometrically similar, consider the Reynolds number to be constant across both valves under the same type of fluid flow conditions. Using the Reynolds number (\(Re\)) and the property of similar flow in geometrically similar devices, the flow rates (\(Q\)) of air through both valves should follow the relation of \(Q_{1} /Q_{2} = (D_{1} / D_{2})^{3}\), where \(D\)'s are the diameters. Here, we don't know the scale factor of enlargement (\(D_{1} /D_{2}\)) yet, hence we cannot proceed directly. We have to consider density difference between water and air for the similar Reynold's number.
03

Account for difference in densities between air and water

The densities (ρ) of air at \(60^{\circ} \mathrm{F}\) and water at \(60^{\circ} \mathrm{F}\) are approximately \(0.002377~\mathrm{slugs/ft}^{3}\) and \(1.94~\mathrm{slugs/ft}^{3}\) respectively. Using the Reynolds number principle, to maintain the Reynold's number constant between air and water, we can relate the diameters using \( D_{1} = D_{2} \times \sqrt[3]{(Q_{air} \times \rho_{air}) / (Q_{water} \times \rho_{water})}\).
04

Calculation of the size

Substituting the known values into the equation from Step 3, \( D_{1} = 1/8 \times \sqrt[3]{(0.005 \times 0.002377) / (Q_{water} \times 1.94)}\). The water flow rate \(Q_{water}\) was previously computed in Step 1. So, the new size relative to initial size can be computed and thus the answer.

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

By inspection, arrange the following dimensional parameters into dimensionless parameters: (a) kinematic viscosity, \(v,\) length, \(\ell,\) and time, \(t ;\) and (b) volume flow rate, \(Q,\) pump diameter, \(D,\) and pump impeller rotation speed, \(N\)

The pressure rise, \(\Delta p,\) across a pump can be expressed as \\[ \Delta p=f(D, \rho, \omega, Q) \\] where \(D\) is the impeller diameter, \(\rho\) the fluid density, \(\omega\) the rotational speed, and \(Q\) the flowrate. Determine a suitable set of dimensionless parameters.

A student drops two spherical balls of different diameters and different densities. She has a stroboscopic photograph showing the positions of each ball as a function of time. However, she wants to express the velocity of each as a function of time in dimensionless form. Develop the dimensionless group. The equation of motion for each ball is $$m g-\frac{C_{D}}{2} \rho A V^{2}=m \frac{d V}{d t}$$ where \(m\) is ball mass, \(g\) is acceleration of gravity, \(C_{D}\) is a dimensionless and constant drag coefficient, \(\rho\) is air mass density, \(A\) is ball cross-sectional area \(\left(=\pi \mathrm{D}^{2} / 4\right)\) with \(D\) ball diameter, \(V\) is ball velocity, and \(t\) is time.

A breakwater is a wall built around a harbor so the incoming waves dissipate their energy against it. The significant dimensionless perameters are the Froude number Frand the Reynolds number Re. A particular breakwater measuring \(450 \mathrm{m}\) long and \(20 \mathrm{m}\) deep is hit by waves \(5 \mathrm{m}\) high and velocities up to \(30 \mathrm{m} / \mathrm{s}\). In a \(\frac{1}{100}\) -scale model of the breakwater, the wave height and velocity can be controlled. Can complete similarity be obtained using water for the model test?

The drag characteristics of an airplane are to be determined by model tests in a wind tunnel operated at an absolute pressure of \(1300 \mathrm{kPa}\). If the prototype is to cruise in standard air at 385 \(\mathrm{km} / \mathrm{hr},\) and the corresponding speed of the model is not o differ by more than \(20 \%\) from this (so that compressibility effects may be ignored), what range of length scales may be used if Reynolds number similarity is to be maintained? Assume the viscosity of air is unaffected by pressure, and the temperature of air in the tunnel is equal to the temperature of the air in which the airplane will fly.

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free