Package: Loose Leaf For Fluid Mechanics With 1 Semester Connect Access Card
Package: Loose Leaf For Fluid Mechanics With 1 Semester Connect Access Card
8th Edition
ISBN: 9781259638848
Author: White
Publisher: MCG
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Chapter 4, Problem 4.1P
To determine

(a)

Whether the flow is steady or unsteady.

Whether the flow is two or three dimensional.

The acceleration vector of the velocity field.

Expert Solution
Check Mark

Answer to Problem 4.1P

The given flow is an unsteady flow.

The flow is a three dimensional flow.

The acceleration vector of the velocity field is a=4[1+4t2]i4t[1t3]j.

Explanation of Solution

Given information:

Write the expression for the idealized velocity field.

V=4txi2t2yj+4xzk

Here, the variables for position are x, y and z, and the variable for time is t.

The given point on the velocity field is (1,1,0).

A unsteady flow is a flow that changes with respect to time.

The given velocity field has a component of time. Hence, the flow is an unsteady flow.

A two dimensional flow is a flow that has two components of velocity and a three dimensional flow has three components of velocity.

As the given flow field has three components of velocity hence, it is a three dimensional flow.

Write the general expression for the velocity field.

V=ui+vj+wk

Here, the velocity function in x-coordinate is u, the velocity function in y-coordinate is v and the velocity component in z-coordinate is w.

Write the expression for the acceleration function along x-coordinate with respect to time.

dudt=ut+uux+vuy+wuz ..... (I)

Here, the velocity gradient of u with respect to x coordinate is ux, the velocity gradient of u with respect to y-coordinate is uy and the velocity gradient of u with respect to z-coordinate is uz.

Write the expression for the acceleration function in y-coordinate with respect to time.

dvdt=vt+uvx+vvy+wvz ..... (II)

Here, the velocity gradient of v with respect to x coordinate is vx, the velocity gradient of v with respect to y-coordinate is vy and the velocity gradient of v with respect to z-coordinate is vz.

Write the expression for the acceleration function in z-coordinate with respect to time.

dwdt=wt+uwx+vwy+wwz ..... (III)

Here, the velocity gradient of w with respect to x coordinate is wx, the velocity gradient of w with respect to y-coordinate is wy and the velocity gradient of w with respect to z-coordinate is wz.

Write the expression for acceleration.

a=(dudt)i+(dvdt)j+(dwdt)k ..... (IV)

Substitute 4xt for u, 2t2y for v and 4xz for w in Equation (I).

dudt=( 4xt)t+(4xt)( 4xt)x+(2t2y)( 4xt)y+(4xz)( 4xt)z=4x+16xt2

Substitute 4xt for u, 2t2y for v and 4xz for w in Equation (II).

dvdt=( 2 t 2 y)t+(4xt)( 2 t 2 y)x+(2t2y)( 2 t 2 y)y+(4xz)( 2 t 2 y)z=4ty+4t4y

Substitute 4xt for u, 2t2y for v and 4xz for w in Equation (III).

dwdt=( 4xz)t+(4xt)( 4xz)x+(2t2y)( 4xz)y+(4xz)( 4xz)z=16xtz+16x2z

Substitute 16xtz+16x2z for dwdt, 4ty+4t4y for dvdt and 4x+16xt2 for dudt in Equation (IV).

a=[4x+16xt2]i+[4ty+4t4y]j+[16xtz+16x2z]k ..... (V)

Calculation:

Substitute 1 for x, 1 for y and 0 for z in Equation (V).

a=[4(1)+16(1)t2]i+[4t(1)+4t4(1)]j+[16(1)t(0)+16( 1)2(0)]k=[416t2]i+[4t+4t4]j=4[1+4t2]i4t[1t3]j

Conclusion:

Thus, the given flow is an unsteady flow.

Thus, the given flow is three-dimensional.

Thus, the acceleration vector of the velocity field is a=4[1+4t2]i4t[1t3]j.

To determine

(b)

The unit vector normal to the acceleration.

Expert Solution
Check Mark

Answer to Problem 4.1P

The unit vector normal to the acceleration is a^n=±[t( t 31)]i+[(1+4 t 2)]j ( 1+4 t 2 )2+ [ t( t 3 1 )]2.

Explanation of Solution

Write the general expression for the acceleration.

a=axi+ayj

Here, the component of acceleration in x-coordinate is ax and the component of acceleration in y-coordinate is ay.

Write the expression for unit vector normal to acceleration.

a^n=±ayiaxjax2+ay2 ..... (VI)

Calculation:

Substitute 4[1+4t2] for ax and 4t[1t3] for ay in Equation (VII).

a^n=±[4t( 1 t 3 )]i[4( 1+4 t 2 )]j [ 4( 1+4 t 2 )]+ [ 4t( 1 t 3 )] 2 =±[t( t 3 1)]i+[( 1+4 t 2 )]j ( 1+4 t 2 ) 2 + [ t( t 3 1 )] 2

Conclusion:

Thus, the unit vector normal to the acceleration is a^n=±[t( t 31)]i+[(1+4 t 2)]j ( 1+4 t 2 )2+ [ t( t 3 1 )]2.

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Chapter 4 Solutions

Package: Loose Leaf For Fluid Mechanics With 1 Semester Connect Access Card

Ch. 4 - Prob. 4.11PCh. 4 - Prob. 4.12PCh. 4 - Prob. 4.13PCh. 4 - Prob. 4.14PCh. 4 - What is the most general form of a purely radial...Ch. 4 - Prob. 4.16PCh. 4 - An excellent approximation for the two-dimensional...Ch. 4 - Prob. 4.18PCh. 4 - A proposed incompressible plane flow in polar...Ch. 4 - Prob. 4.20PCh. 4 - Prob. 4.21PCh. 4 - Prob. 4.22PCh. 4 - Prob. 4.23PCh. 4 - Prob. 4.24PCh. 4 - An incompressible flow in polar coordinates is...Ch. 4 - Prob. 4.26PCh. 4 - Prob. 4.27PCh. 4 - P4.28 For the velocity distribution of Prob. 4.10,...Ch. 4 - Prob. 4.29PCh. 4 - Prob. 4.30PCh. 4 - Prob. 4.31PCh. 4 - Prob. 4.32PCh. 4 - Prob. 4.33PCh. 4 - Prob. 4.34PCh. 4 - P4.35 From the Navier-Stokes equations for...Ch. 4 - A constant-thickness film of viscous liquid flows...Ch. 4 - Prob. 4.37PCh. 4 - Prob. 4.38PCh. 4 - Reconsider the angular momentum balance of Fig....Ch. 4 - Prob. 4.40PCh. 4 - Prob. 4.41PCh. 4 - Prob. 4.42PCh. 4 - Prob. 4.43PCh. 4 - Prob. 4.44PCh. 4 - Prob. 4.45PCh. 4 - Prob. 4.46PCh. 4 - Prob. 4.47PCh. 4 - Consider the following two-dimensional...Ch. 4 - Prob. 4.49PCh. 4 - Prob. 4.50PCh. 4 - Prob. 4.51PCh. 4 - Prob. 4.52PCh. 4 - Prob. 4.53PCh. 4 - P4.54 An incompressible stream function is...Ch. 4 - Prob. 4.55PCh. 4 - Prob. 4.56PCh. 4 - A two-dimensional incompressible flow field is...Ch. 4 - P4.58 Show that the incompressible velocity...Ch. 4 - Prob. 4.59PCh. 4 - Prob. 4.60PCh. 4 - An incompressible stream function is given by...Ch. 4 - Prob. 4.62PCh. 4 - Prob. 4.63PCh. 4 - Prob. 4.64PCh. 4 - Prob. 4.65PCh. 4 - Prob. 4.66PCh. 4 - A stream function for a plane, irrotational, polar...Ch. 4 - Prob. 4.68PCh. 4 - A steady, two-dimensional flow has the following...Ch. 4 - A CFD model of steady two-dimensional...Ch. 4 - Consider the following two-dimensional function...Ch. 4 - Prob. 4.72PCh. 4 - Prob. 4.73PCh. 4 - Prob. 4.74PCh. 4 - Given the following steady axisymmetric stream...Ch. 4 - Prob. 4.76PCh. 4 - Prob. 4.77PCh. 4 - Prob. 4.78PCh. 4 - Prob. 4.79PCh. 4 - Oil, of density and viscosity , drains steadily...Ch. 4 - Prob. 4.81PCh. 4 - Prob. 4.82PCh. 4 - P4.83 The flow pattern in bearing Lubrication can...Ch. 4 - Consider a viscous film of liquid draining...Ch. 4 - Prob. 4.85PCh. 4 - Prob. 4.86PCh. 4 - Prob. 4.87PCh. 4 - The viscous oil in Fig. P4.88 is set into steady...Ch. 4 - Oil flows steadily between two fixed plates that...Ch. 4 - Prob. 4.90PCh. 4 - Prob. 4.91PCh. 4 - Prob. 4.92PCh. 4 - Prob. 4.93PCh. 4 - Prob. 4.94PCh. 4 - Two immiscible liquids of equal thickness h are...Ch. 4 - Prob. 4.96PCh. 4 - Prob. 4.97PCh. 4 - Prob. 4.98PCh. 4 - For the pressure-gradient flow in a circular tube...Ch. 4 - W4.1 The total acceleration of a fluid particle is...Ch. 4 - Is it true that the continuity relation, Eq....Ch. 4 - Prob. 4.3WPCh. 4 - Prob. 4.4WPCh. 4 - W4.5 State the conditions (there are more than...Ch. 4 - Prob. 4.6WPCh. 4 - W4.7 What is the difference between the stream...Ch. 4 - Under what conditions do both the stream function...Ch. 4 - Prob. 4.9WPCh. 4 - Consider an irrotational, incompressible,...Ch. 4 - Prob. 4.1FEEPCh. 4 - Prob. 4.2FEEPCh. 4 - Prob. 4.3FEEPCh. 4 - Given the steady, incompressible velocity...Ch. 4 - Prob. 4.5FEEPCh. 4 - Prob. 4.6FEEPCh. 4 - C4.1 In a certain medical application, water at...Ch. 4 - Prob. 4.2CP
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