Fluid Mechanics, 8 Ed
Fluid Mechanics, 8 Ed
8th Edition
ISBN: 9789385965494
Author: Frank White
Publisher: MCGRAW-HILL HIGHER EDUCATION
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Chapter 4, Problem 4.30P
To determine

(a)

The validation of continuity equation.

Expert Solution
Check Mark

Answer to Problem 4.30P

The continuity equation is valid for the given velocity distribution.

Explanation of Solution

Given information:

Two dimensional converging nozzle velocity distribution in x direction, y direction and z direction is u=Uo1+xL, v=UoyL, w=0 respectively. Here, the velocity in x -direction is u, velocity, the velocity in y -direction is v . the velocity in z direction is w.

Write the expression for two dimensional incompressible continuity Equation.

ux+vy=0 ... (I)

Here, the velocity of fluid along x and y directions are u and v respectively, Velocity component along x direction is ux, Velocity component along y direction is vy.

Calculation:

Substitute Uo1+xL for u, UoyL for v, in Equation (I).

xUo 1+ x L +yUoyL=0Uo 0+ 1 L +Uo1L=0UoLUoL=0

Conclusion:

The given distribution satisfies the two dimensional continuity equation..

To determine

(b)

The validation of Navier stokes equation.

Expert Solution
Check Mark

Answer to Problem 4.30P

Navier stokes equation is valid for the the given velocity distribution.

Explanation of Solution

Write the expression for two dimensional incompressible Navier stoke equation in x direction.

uux+vuy=1ρpx+v2ux2+2vy2 ... (II)

Write the expression for two dimensional incompressible Navier stoke equation in y direction.

uvx+vvy=1ρpy+v2vx2+2vy2 ... (III)

Here, the velocity of fluid along x and y directions are u and v respectively, Velocity component along x direction is ux, Velocity component along y direction is vy

Write the expression for validation for Navier stokes equation in x-direction.

2pxy=xpy=0 ... (IV)

Write the expression for validation for Navier stokes equation in y-direction.

2pyx=ypx=0 ... (V)

Calculation:

Substitute Uo1+xL for u, UoyL for v, 0 for 2ux2, 0 for 2uy2 in Equation (II).

U o 1+ x L U o 1+ x L x + U o y L U o 1+ x L y =1ρpx+v0+0Uo 1+ x L U o L + U o y L 0=1ρpx+0 U o 2 L 1+ x L +0=1ρpxρ U o 2 L1+xL=px

px=ρUo2L1+xL ... (VI)

Substitute Uo1+xL for u, UoyL for v, 0 for 2ux2, 0 for 2uy2 in Equation (III).

Uo 1+ x L U o y L x+UoyL U o y L y=1ρpy+v0+0Uo1+xL0+UoyLUo1L=1ρpy+00+ U o 2 y L 2 =1ρpyρ U o 2 y L 2 =py

py=ρUo2yL2 ... (VII)

Substitute ρUo2yL2 for py in Equation (IV).

xρ U o 2 y L 2 =00=0

Hence the equation v=UoyL has an exact solution to Navier stokes

Substitute ρUo2L1+xL for px in Equation (V).

y ρ U o 2 L 1+ x L =00=0

Hence the equation u=Uo1+xL has an exact solution to Navier stokes

Conclusion:

Navier stokes equation is valid for the given velocity distribution.

To determine

(c)

The pressure distribution p(x,y).

Expert Solution
Check Mark

Answer to Problem 4.30P

The pressure distribution p(x,y) is ρUo2Lx+x22L+y22L+po

Explanation of Solution

Given information:

The pressure at the origin is pa.

Write the expression for pressure distribution in x direction.

px=pxdx ... (VIII)

Write the expression for pressure distribution in y direction.

py=pydy ... (IX)

Write the expression for pressure distribution

p=px+py ... (X)

Calculation:

Substitute ρUo2L1+xL for px in Equation (VIII).

px= ρ U o 2 L 1+ x L dx= ρ U o 2 Lx+ x 2 2L ... (XI)

Substitute ρUo2yL2 for py in Equation (IX).

py= ρ U o 2 y L 2 dy=ρUo2 y 2 2 L 2 +C ... (XII)

Substitute pa for C in Equation (XII).

ρUo2y22L2+Pa

Substitute ρUo2Lx+x22L for px and ρUo2y22L2+Pa for py in Equation (X)

p= ρ U o 2 Lx+ x 2 2LρUo2 y 2 2 L 2 +Pa=ρUo2Lx+ x 2 2L+ y 2 2 L 2 +Pa

Conclusion:

The pressure field p(x,y) is ρUo2Lx+x22L+y22L2+Pa.

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Chapter 4 Solutions

Fluid Mechanics, 8 Ed

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