FLUID MECHANICS FUNDAMENTALS+APPS
FLUID MECHANICS FUNDAMENTALS+APPS
4th Edition
ISBN: 9781259877766
Author: CENGEL
Publisher: MCG
bartleby

Concept explainers

bartleby

Videos

Textbook Question
Book Icon
Chapter 4, Problem 66P

Consider steady, incompressible, two-dimensional shear flow for which the velocity field is V = ( u , v ) = ( a + b y ) i + 0 j where a and b are constants. Sketched in Fig. P4-66 is a small rectangular fluid particle of dimensions dx and dy at time t. The fluid particle moves and deforms with the flow such that at a later time (t + dt), the particle is no longer rectangular, as also shown in the figure. The initial location of each corner of the fluid particle is labeled in Fig. P4-66. The lower-left corner is at (x,y) at time t, where the x-component of velocity is u = a +by. At the later time, this corner moves to (x + u dt, y), or ( x + ( a + b y ) d t , y )
(a) In similar fashion, calculate the location of each of the other three corners of the fluid particle at time t+dt.
(b) From the fundamental definition of linear strain rate (the rate of increase in length per unit length), calculate linear strain rates ε x x and ε y y .
(c) Compare your results with those obtained from the equations for ε x x and ε y y in Cartesian coordinates. i.e.,
   ε x x = u x ε y y = u y

Expert Solution
Check Mark
To determine

(a)

The location of each of the other three corners of the fluid particle at time t+dt.

Answer to Problem 66P

The location of the lower left corner after time t+dt is [(x+(a+by)dt),y].

The location of the lower right corner after time t+dt is [(x+(a+by)dt+dx),y].

The location of the upper left corner after time t+dt is [(x+(a+b( y+dy))dt),(y+dy)].

The location of the upper right corner after time t+dt is [(x+dx+(a+b( y+dy))dt+dx),(y+dy)].

Explanation of Solution

Given information:

Two-dimensional shear flow, flow is incompressible, the velocity field is (a+by)i+0j, dimension of the fluid particle at the initial time is dx, and dy and initial x component of the velocity is a+by.

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

  V=(a+by)i+0j   ...... (I)

Here, the constants are a and b, the distance in x direction is x and the distance in y direction is y.

The following figure shows the position of the corners at time t and t+dt.

  FLUID MECHANICS FUNDAMENTALS+APPS, Chapter 4, Problem 66P

Figure-(1)

Here, the length of the lower edge at time t is dx, length of the left edge at time t is dy, length of the lower edge at time t+dt is n, and the length of the right edge at time t+dt is m.

Write the expression for location of the lower left corner after time t+dt.

  A=[(x+udt),y]   ...... (II)

Write the expression for location of the lower right corner after time t+dt.

  B=[(x+udt+dx),y]   ...... (III)

Write the expression for location of the upper left corner after time t+dt.

  C=[(x+udt),(y+dy)]   ...... (IV)

Write the expression for location of the upper right corner after time t+dt.

  D=[(x+dx+udt+dx),(y+dy)]   ...... (V)

Write the expression for velocity along x direction.

  u=a+by   ...... (VI)

Calculation:

Substitute a+by for u in Equation (II).

  A=[(x+(a+by)dt),y]

Substitute a+by for u in Equation (III).

  B=[(x+(a+by)dt+dx),y]

Substitute a+b(y+dy) for u in Equation (IV).

  C=[(x+(a+b( y+dy))dt),(y+dy)]

Substitute a+b(y+dy) for u in Equation (V).

  D=[(x+dx+(a+b( y+dy))dt+dx),(y+dy)]

Conclusion:

The location of the lower left corner after time t+dt is [(x+(a+by)dt),y].

The location of the lower right corner after time t+dt is [(x+(a+by)dt+dx),y].

The location of the upper left corner after time t+dt is [(x+(a+b( y+dy))dt),(y+dy)].

The location of the upper right corner after time t+dt is [(x+dx+(a+b( y+dy))dt+dx),(y+dy)].

Expert Solution
Check Mark
To determine

(b)

The linear strain rates.

Answer to Problem 66P

The linear strain rate along x axis is 0.

The linear strain rate along y axis is 0.

Explanation of Solution

Write the expression for the strain rate along x direction.

  εxx=1dt[ndxdx]   ...... (VII)

Write the expression for the strain rate along y direction.

  εyy=1dt[mdydy]  ...... (VIII)

Write the expression for the length of the lower edge at time t+dt.

  n=[x+udt+dx][x+udt]   ...... (IX)

Write the expression for the length of the lower edge at time t+dt.

  m=[y+dy]ym=dy   ...... (X)

Calculation:

Substitute a+by for u in Equation (IX).

  n=[x+(a+by)dt+dx][x+(a+by)dt]=[x+(a+by)dt+dx]x(a+by)dt=dx

Substitute dx for n in Equation (VII).

  εxx=1dt[dxdxdx]=1dt[0dx]=0

Substitute dy for m in Equation (VIII).

  εyy=1dt[dydydy]=1dt[0dy]=0

Conclusion:

The linear strain rate along x axis is 0.

The linear strain rate along y axis is 0.

Expert Solution
Check Mark
To determine

(c)

The linear strain rates in Cartesian coordinates.

Comparison of the linear strain rate by fundamental principal to the linear strain rates in Cartesian coordinates.

Answer to Problem 66P

The linear strain rate in Cartesian coordinates along x axis is 0.

The linear strain rate in Cartesian coordinates along y axis is 0.

The linear strain rate by fundamental principal and the linear strain rates in Cartesian coordinates are same

Explanation of Solution

Given information:

Linear strain along x axis is ux and linear strain along y axis is vy.

Write the expression for the velocity along y direction.

  v=0   ...... (XI)

Write the expression for the linear strain rate along x direction in Cartesian coordination.

  εxx=ux   ...... (XII)

Write the expression for the linear strain rate along y direction in Cartesian coordination.

  εyy=vy   ...... (XIII)

Calculation:

Substitute a+by for u in Equation (XII).

  εxx=x(a+by)=0

Substitute 0 for v in Equation (XIII).

  εyy=y(0)=0

Conclusion:

The linear strain rate in Cartesian coordinates along x axis is 0.

The linear strain rate in Cartesian coordinates along y axis is 0.

The linear strain rate by fundamental principal and the linear strain rates in Cartesian coordinates are the same.

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
4-17 Converging duct flow is modeled by the steady, two-dimensional velocity field of Prob. 4-16. The pressure field is given by P = Po 2U,bx + b°(x² + y°) where P, is the pressure at x = 0. Generate an expression for the rate of change of pressure following a fluid particle.
For a certain two-dimensional incompressible flow, velocity field is given by 2xy î - y?j. The streamlines for this flow are given by the family of curves
Consider fully developed Couette flow between two infinite parallel plates separated by distance h, with the top plate moving and the bottom plate stationary, as illustrated in the figure below. The flow is steady, incompressible, and two-dimensional in the XY plane. The velocity field is given by V }i = (u, v) = (v² )i +0j = V (a) Find out the acceleration field of this flow. (b) Is this flow steady? What are the u and v components of velocity? u= V² h

Chapter 4 Solutions

FLUID MECHANICS FUNDAMENTALS+APPS

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