Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

A horizontal segment of pipe tapers from a cross sectional area of $50.0 \mathrm{cm}^{2}\( to \)0.500 \mathrm{cm}^{2} .$ The pressure at the larger end of the pipe is \(1.20 \times 10^{5} \mathrm{Pa}\) and the speed is $0.040 \mathrm{m} / \mathrm{s} .$ What is the pressure at the narrow end of the segment?

Short Answer

Expert verified
Answer: The pressure at the narrow end of the pipe segment is approximately \(1.12 \times 10^5\, \mathrm{Pa}\).

Step by step solution

01

Find the speed of the fluid at the narrow end of the pipe

According to the principle of continuity, the product of the cross-sectional area and the speed of the fluid remains constant throughout the pipe. So: \(A_1v_1 = A_2v_2\) Here, \(A_1 = 50.0 \,\mathrm{cm}^2 = 5.0 \times 10^{-2} \,\mathrm{m}^2\), \(v_1 = 0.040\, \mathrm{m/s}\), and \(A_2 = 0.500\, \mathrm{cm}^2 = 5.0 \times 10^{-4} \,\mathrm{m}^2\). We will solve for \(v_2\): \(v_2 =\dfrac{A_1v_1}{A_2} = \dfrac{(5.0 \times 10^{-2} \,\mathrm{m}^2)(0.040\, \mathrm{m/s})}{5.0 \times 10^{-4} \,\mathrm{m}^2} = 4\, \mathrm{m/s}\)
02

Apply Bernoulli's equation to find the pressure at the narrow end

Bernoulli's equation states that the total mechanical energy per unit volume remains constant along a streamline, so: \(P_1 + \dfrac{1}{2} \rho v_1^2 = P_2 + \dfrac{1}{2} \rho v_2^2\) Here, \(P_1 = 1.20 \times 10^5\, \mathrm{Pa}\), \(v_1 = 0.040\, \mathrm{m/s}\), and \(v_2 = 4\, \mathrm{m/s}\). The fluid is not specified, but we can assume it's water, with \(\rho = 1000\, \mathrm{kg/m^3}\). We will solve for \(P_2\): \(P_2 = P_1 + \dfrac{1}{2} \rho v_1^2 - \dfrac{1}{2} \rho v_2^2\) \(P_2 = 1.20 \times 10^5\, \mathrm{Pa} + \dfrac{1}{2} (1000\, \mathrm{kg/m^3})(0.040\, \mathrm{m/s})^2 - \dfrac{1}{2} (1000\, \mathrm{kg/m^3})( 4\, \mathrm{m/s})^2\) \(P_2 = 1.20 \times 10^5\, \mathrm{Pa} + 0.8\, \mathrm{Pa} - 8000\, \mathrm{Pa}\) \(P_2 = 1.20 \times 10^5\, \mathrm{Pa} - 7.1992 \times 10^3\, \mathrm{Pa}\) \(P_2 \approx 1.12 \times 10^5\, \mathrm{Pa}\) So the pressure at the narrow end of the pipe segment is approximately \(1.12 \times 10^5\, \mathrm{Pa}\).

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

The maximum pressure most organisms can survive is about 1000 times atmospheric pressure. Only small, simple organisms such as tadpoles and bacteria can survive such high pressures. What then is the maximum depth at which these organisms can live under the sea (assuming that the density of seawater is \(1025 \mathrm{kg} / \mathrm{m}^{3}\) )?

An airplane flies on a level path. There is a pressure difference of 500 Pa between the lower and upper surfaces of the wings. The area of each wing surface is about \(100 \mathrm{m}^{2} .\) The air moves below the wings at a speed of \(80.5 \mathrm{m} / \mathrm{s} .\) Estimate (a) the weight of the plane and (b) the air speed above the wings.
The deepest place in the ocean is the Marianas Trench in the western Pacific Ocean, which is over \(11.0 \mathrm{km}\) deep. On January \(23,1960,\) the research sub Trieste went to a depth of \(10.915 \mathrm{km},\) nearly to the bottom of the trench. This still is the deepest dive on record. The density of seawater is \(1025 \mathrm{kg} / \mathrm{m}^{3} .\) (a) What is the water pressure at that depth? (b) What was the force due to water pressure on a flat section of area \(1.0 \mathrm{m}^{2}\) on the top of the sub's hull?
(a) since the flow rate is proportional to the pressure difference, show that Poiseuille's law can be written in the form \(\Delta P=I R,\) where \(I\) is the volume flow rate and \(R\) is a constant of proportionality called the fluid flow resistance. (Written this way, Poiseuille's law is analogous to Ohm's law for electric current to be studied in Chapter \(18: \Delta V=I R,\) where \(\Delta V\) is the potential drop across a conductor, \(I\) is the electric current flowing through the conductor, and \(R\) is the electrical resistance of the conductor.) (b) Find \(R\) in terms of the viscosity of the fluid and the length and radius of the pipe.
A viscous liquid is flowing steadily through a pipe of diameter \(D .\) Suppose you replace it by two parallel pipes, each of diameter \(D / 2,\) but the same length as the original pipe. If the pressure difference between the ends of these two pipes is the same as for the original pipe, what is the total rate of flow in the two pipes compared to the original flow rate?
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