Fluid Mechanics: Fundamentals and Applications
Fluid Mechanics: Fundamentals and Applications
4th Edition
ISBN: 9781259696534
Author: Yunus A. Cengel Dr., John M. Cimbala
Publisher: McGraw-Hill Education
bartleby

Concept explainers

bartleby

Videos

Question
Book Icon
Chapter 4, Problem 52P
To determine

The expression for the change in length of the line segment.

Expert Solution & Answer
Check Mark

Answer to Problem 52P

The expression for the change in length of the line segment is (xBxA)(ebt1).

Explanation of Solution

Given information:

The flow is symmetric about x axis.

Write the expression for the two-dimensional velocity field in the vector form.

  V=(U0+bx)ibyj   ...... (I)

Here, the horizontal speed is U0, the constant is b and the distance in x direction is x and the distance in y direction is y.

Write the expression for the velocity component along x direction.

  u=U0+bx  ...... (II)

Here, the variable is x in x direction.

Write the expression for the velocity component along x direction.

  v=by   ...... (III)

Here, the variable is y in y direction.

Write the expression for the velocity in x direction in differential form.

  dxdt=u   ...... (IV)

Write the expression for the initial length.

  ζ=xBxA  ...... (V)

Here, the initial location of A is xA and the initial location of B is xB.

Write the expression for the final length.

  ζ+Δζ=xBxA   ...... (VI)

Here, the final location of A is xA, the final location of B is xB the change in length is Δζ.

Write the expression for the change in lengths.

  Δζ=(ζ+Δζ)ζ   ...... (VII)

Calculation:

Substitute U0+bx for u in Equation (IV).

  dxdt=U0+bxdxU0+bx=dt   ...... (VIII)

Integrate the Equation (VIII).

   dx U 0 +bx=dt1bln(U0+bx)=tlnC1ln(U0+bx)1b+lnC1=tt=C1ln(U0+bx)1b  ...... (IX)

Substitute xA for x and 0 for t in Equation (IX).

  0=C1ln(U0+bxA)1bln(1)=ln[C1( U 0 +b x A )1b]C1(U0+bxA)1b=1C1=1( U 0 +b x A ) 1 b

Substitute 1( U 0+b x A)1b for C1 in Equation (IX).

  t=ln(1 ( U 0 +b x A ) 1 b ( U 0 +bx) 1 b)t=1bln( U 0+bx U 0+b x A)bt=ln( U 0+bx U 0+b x A)ebt=( U 0+bx U 0+b x A)

  ebt(U0+bxA)=(U0+bx)x=1b[(U0+bxA)ebtU0]xA=1b[(U0+bxA)ebtU0]xB=1b[(U0+bxB)ebtU0]

Substitute xBxA for ζ+Δζ and xBxA for ζ in Equation (VII).

  Δζ=(xBxA)(xBxA)   ...... (X)

Substitute 1b[(U0+bxB)ebtU0] for xB and 1b[(U0+bxA)ebtU0] for xA in Equation (X).

  Δζ=(1b[( U 0 +b x B )e btU0]1b[( U 0 +b x A )e btU0])(xBxA)=(1b[( U 0 +b x B )e btU0( U 0 +b x A )e bt+U0])(xBxA)=(xBxA)ebt(xBxA)=(xBxA)(ebt1)

Conclusion:

The expression for the change in length of the line segment is (xBxA)(ebt1).

Want to see more full solutions like this?

Subscribe now to access step-by-step solutions to millions of textbook problems written by subject matter experts!
Students have asked these similar questions
The radial velocity component in a incomplreesible, two-dimensional steady flow field (v2=0) is in the figure. Determine the acceleration field a(->) (r,θ)
The stream function in a two-dimensional flow field is given by y=x²- y². Then the magnitude of velocity at point (1, 1) is
The velocity field for an incompressible flow is given as                                 V-›= 5x2i-›− 20 xyj-›+100t k-›.                                                               Determine if this flow is steady. Also determine the velocity and acceleration of a particle at (l, 3, 3) at t = 0.2 s.

Chapter 4 Solutions

Fluid Mechanics: Fundamentals and Applications

Ch. 4 - Define a steady flow field in the Eulerian...Ch. 4 - Is the Eulerian method of fluid flow analysis more...Ch. 4 - A weather balloon is hunched into the atmosphere...Ch. 4 - A Pilot-stalk probe can often be seen protruding...Ch. 4 - List at least three oiler names for the material...Ch. 4 - Consider steady, incompressible, two-dimensional...Ch. 4 - Converging duct flow is modeled by the steady,...Ch. 4 - A steady, incompressible, two-dimensional velocity...Ch. 4 - A steady, incompressible, two-dimensional velocity...Ch. 4 - For the velocity field of Prob. 4-6, calculate the...Ch. 4 - Consider steady flow of air through the diffuser...Ch. 4 - For the velocity field of Prob. 4-21, calculate...Ch. 4 - A steady, incompressible, two-dimensional (in the...Ch. 4 - The velocity field for a flow is given by...Ch. 4 - Prob. 25CPCh. 4 - What is the definition of a timeline? How can...Ch. 4 - What is the definition of a streamline? What do...Ch. 4 - Prob. 28CPCh. 4 - Consider the visualization of flow over a 15°...Ch. 4 - Consider the visualization of ground vortex flow...Ch. 4 - Consider the visualization of flow over a sphere...Ch. 4 - Prob. 32CPCh. 4 - Consider a cross-sectional slice through an array...Ch. 4 - A bird is flying in a room with a velocity field...Ch. 4 - Conversing duct flow is modeled by the steady,...Ch. 4 - The velocity field of a flow is described by...Ch. 4 - Consider the following steady, incompressible,...Ch. 4 - Consider the steady, incompressible,...Ch. 4 - A steady, incompressible, two-dimensional velocity...Ch. 4 - Prob. 41PCh. 4 - Prob. 42PCh. 4 - The velocity field for a line some in the r plane...Ch. 4 - A very small circular cylinder of radius Rtis...Ch. 4 - Consider the same two concentric cylinders of...Ch. 4 - The velocity held for a line vartex in the r...Ch. 4 - Prob. 47PCh. 4 - Name and briefly describe the four fundamental...Ch. 4 - Prob. 49CPCh. 4 - Prob. 50PCh. 4 - Prob. 51PCh. 4 - Prob. 52PCh. 4 - Prob. 53PCh. 4 - Converging duct flow is modeled by the steady,...Ch. 4 - Converging duct flow is modeled by the steady,...Ch. 4 - Using the results of Prob. 4—57 and the...Ch. 4 - Converging duct flow (Fig. P4—16) is modeled by...Ch. 4 - Prob. 60PCh. 4 - For the velocity field of Prob. 4—60, what...Ch. 4 - For the velocity field of Prob. 4—60, calculate...Ch. 4 - For the velocity field of Prob. 4—60, calculate...Ch. 4 - Prob. 64PCh. 4 - Prob. 65PCh. 4 - Consider steady, incompressible, two-dimensional...Ch. 4 - Prob. 67PCh. 4 - Consider the steady, incompressible,...Ch. 4 - Prob. 69PCh. 4 - Prob. 70PCh. 4 - Prob. 71PCh. 4 - Prob. 72PCh. 4 - Prob. 73PCh. 4 - A cylindrical lank of water rotates in solid-body...Ch. 4 - Prob. 75PCh. 4 - A cylindrical tank of radius rrim= 0.354 m rotates...Ch. 4 - Prob. 77PCh. 4 - Prob. 78PCh. 4 - Prob. 79PCh. 4 - For the Couette flow of Fig. P4—79, calculate the...Ch. 4 - Combine your results from Prob. 4—80 to form the...Ch. 4 - Consider a steady, two-dimensional, incompressible...Ch. 4 - A steady, three-dimensional velocity field is...Ch. 4 - Consider the following steady, three-dimensional...Ch. 4 - Prob. 85PCh. 4 - A steady, three-dimensional velocity field is...Ch. 4 - Briefly explain the purpose of the Reynolds...Ch. 4 - Prob. 88CPCh. 4 - True or false: For each statement, choose whether...Ch. 4 - Consider the integral ddtt2tx2. Solve it two ways:...Ch. 4 - Prob. 91PCh. 4 - Consider the general form of the Reynolds...Ch. 4 - Consider the general form of the Reynolds...Ch. 4 - Prob. 94PCh. 4 - Prob. 95PCh. 4 - Prob. 96PCh. 4 - Prob. 97PCh. 4 - The velocity field for an incompressible flow is...Ch. 4 - Consider fully developed two-dimensional...Ch. 4 - For the two-dimensional Poiseuille flow of Prob....Ch. 4 - Combine your results from Prob. 4—100 to form the...Ch. 4 - Prob. 103PCh. 4 - Prob. 107PCh. 4 - Prob. 108PCh. 4 - Prob. 109PCh. 4 - Prob. 110PCh. 4 - Prob. 112PCh. 4 - Prob. 113PCh. 4 - Prob. 114PCh. 4 - Prob. 116PCh. 4 - Based on your results of Prob. 4—116, discuss the...Ch. 4 - Prob. 118PCh. 4 - In a steady, two-dimensional flow field in the...Ch. 4 - A steady, two-dimensional velocity field in the...Ch. 4 - A velocity field is given by u=5y2,v=3x,w=0 . (Do...Ch. 4 - The actual path traveled by an individual fluid...Ch. 4 - Prob. 123PCh. 4 - Prob. 124PCh. 4 - Prob. 125PCh. 4 - Water is flowing in a 3-cm-diameter garden hose at...Ch. 4 - Prob. 127PCh. 4 - Prob. 128PCh. 4 - Prob. 129PCh. 4 - Prob. 130PCh. 4 - Prob. 131PCh. 4 - An array of arrows indicating the magnitude and...Ch. 4 - Prob. 133PCh. 4 - Prob. 134PCh. 4 - Prob. 135PCh. 4 - A steady, two-dimensional velocity field is given...Ch. 4 - Prob. 137PCh. 4 - Prob. 138PCh. 4 - Prob. 139PCh. 4 - Prob. 140PCh. 4 - Prob. 141P
Knowledge Booster
Background pattern image
Mechanical Engineering
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.
Similar questions
SEE MORE QUESTIONS
Recommended textbooks for you
Text book image
Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press
Text book image
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON
Text book image
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education
Text book image
Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY
Text book image
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning
Text book image
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY
Introduction to Kinematics; Author: LearnChemE;https://www.youtube.com/watch?v=bV0XPz-mg2s;License: Standard youtube license