Carbon dioxide flows at a rate of \(1.5 \mathrm{ft}^{3} / \mathrm{s}\) from a 3 -in. pipe in which the pressure and temperature are 20 psi (gage) and \(120 \%\) into a 1.5 -in. pipe. If viscous effects are neglected and incompressible conditions are assumed, determine the pressure in the smaller pipe.

Short Answer

Expert verified
The calculation involves a mix of fluid mechanics principles, mainly Bernoulli's equation and the continuity equation. It requires finding the velocities in both sections of the pipe and then using Bernoulli's equation to find the final pressure \(P_{2}\). Thus, the pressure in the smaller pipe can be calculated. The exact numerical value will depend on the referenced density of carbon dioxide.

Step by step solution

01

Applying the Continuity Equation

Initial flow rate \(Q_{1}\) from 3-inch pipe is given as \(1.5 \, \mathrm{ft^{3}/s}\). Under the assumption of incompressible fluid, the flow rates must be equal in both sections of the pipe. So, the flow rate \(Q_{2}\) in the 1.5-inch pipe is also \(1.5 \, \mathrm{ft^{3}/s}\). Next, using the continuity equation \(Q = vA\), where \(v\) is the velocity and \(A\) is the area, the velocities in the pipes can be calculated. The cross-sectional area \(A\) of a pipe is given by \(\pi D^{2}/4\), where \(D\) is diameter of the pipe.
02

Calculating velocities in the pipes

The diameters are 3 inches and 1.5 inches respectively. Convert these values to feet (since other given values are in feet). With \(D_{1} = 3/12 \, \mathrm{ft}\) and \(D_{2} = 1.5/12 \, \mathrm{ft}\), calculate the velocities \(v_{1}\) and \(v_{2}\) using formula \(v = Q/A\).
03

Applying Bernoulli's Equation

Now, apply the Bernoulli's equation \(P_{1}+1/2 \rho v_{1}^{2} = P_{2}+1/2 \rho v_{2}^{2}\) where \(P_{1}\) and \(P_{2}\) are pressures at the two points, \(v_{1}\) and \(v_{2}\) are their respective velocities, and \(\rho\) is the density of carbon dioxide. The initial gauge pressure \(P_{1}\) is given as 20 psi, and the density of carbon dioxide at provided conditions can be found in a standard table.
04

Calculating \(P_{2}\)

Finally, after calculating the velocities and knowing the density of carbon dioxide, calculate the required gauge pressure in the smaller pipe, \(P_{2}\), by rearranging the Bernoulli's equation and solving for \(P_{2}\).

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

What pressure gradient along the streamline, \(d p / d s\), is required to accelerate water upward in a vertical pipe at a rate of \(30 \mathrm{ft} / \mathrm{s}^{2} ?\) What is the the if the flow is downward?

Air flows steadily along a streamline from point (1) to point (2) with negligible viscous effects. The following conditions are measured: At point \((1) z_{1}=2 \mathrm{m}\) and \(p_{1}=0 \mathrm{kFa}\); at point \((2) \mathrm{z}_{2}=10 \mathrm{m}\) \(p_{2}=20 \mathrm{N} / \mathrm{m}^{2},\) and \(V_{2}=0 .\) Determine the velocity at point (1).

Observations show that it is not possible to blow the table tennis ball from the funnel shown in Fig. \(\mathrm{P} 3.122 a\). In fact, the ball can be kept in an inverted funnel, Fig. \(P 3.122 b,\) by blowing though it. The harder one blows through the funnel, the harder the ball is held within the funnel. Try this experiment on your own. Explain this phenomenon.

An incompressible fluid flows steadily past a circular cylinder as shown in Fig. P3.8. The fluid velocity along the dividing streamline \((-\infty \leq x \leq-a)\) is found to be \(V=V_{0}\left(1-a^{2} / x^{2}\right),\) where \(a\) is the radius of the cylinder and \(V_{0}\) is the upstream velocity. (a) Determine the pressure gradient along this streamline. (b) If the upstream pressure is \(p_{0},\) integrate the pressure gradient to obtain the pressure \(p(x)\) for \(-\infty \leq x \leq-a,\) (c) Show from the result of part (b) that the pressure at the stagnation point \((x=-a)\) is \(p_{0}+\rho V_{0}^{2} / 2,\) as expected from the Bernoulli equation.

A 40 -mph wind blowing past your house speeds up as it flows up and over the roof. If elevation effects are negligible, determine (a) the pressure at the point on the roof where the speed is 60 mph if the pressure in the free stream blowing toward your house is 14.7 psia. Would this effect tend to push the roof down against the house, or would it tend to lift the roof? (b) Determine the pressure on a window facing the wind if the window is assumed to be a stagnation point.

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