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
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Chapter 9, Problem 87P

Consider steady, two-dimensional, incompressible flow due to a spiraling line vortex/sink flow centered on the z-axis. Streamlines and velocity components are shown in Fig. 9-87. The velocity field is u r = C / r and u θ = K / r , where C and K are constants. Calculate the pressure as a function of r and θ .

Chapter 9, Problem 87P, Consider steady, two-dimensional, incompressible flow due to a spiraling line vortex/sink flow
FIGURE P9-87

Expert Solution & Answer
Check Mark
To determine

The pressure field as a function r and θ.

Answer to Problem 87P

The pressure field as a function r and θ is 12ρ(C2+K2r2)+C1.

Explanation of Solution

Given information:

The flow is steady, two-dimensional and incompressible.

The velocity components are ur=Cr and uθ=Kr.

Here, C and K are constants.

Write the expression for continuity equation.

  1r(rur)r+1r(uθ)θ=0........... (I)

Here, velocity components are ur and uθ, radius is r and angle is θ.

Write the expression for the θ -component of Navier-Stokes equation.

  [ρ( u θ t+ u r u θ r+ u θ r u θ θ+ u r u θ r)]=[1rPθ+μ( 1 r r( r u θ r ) u θ r 2 + 1 r 2 2 u θ θ 2 2 r 2 u r θ)+ρgθ]........... (II)

Here, density is ρ, time is t, dynamic viscosity is μ and gravitational acceleration in θ -direction is gθ.

Write the expression for the r -component of Navier-Stokes equation.

  [ρ( u r t+ u r u r r+ u θ r u r θ u θ 2 r)]=[Pr+μ( 1 r r( r u r r ) u r r 2 + 1 r 2 2 u r θ 2 2 r 2 u θ θ)+ρgr]........... (III)

Calculation:

Substitute Cr for ur and Kr for uθ in Equation (I).

  1r( r( C r ))r+1r( K r )θ=01rr(C)+1rθ(Kr)=00+0=00=0........... (IV)

Since both sides of Equation (IV) are equal, therefore continuity equation is verified.

Substitute Cr for ur, 0 for gθ and Kr for uθ in Equation (II).

[ ρ( ( K r ) t +( C r ) ( K r ) r + ( K r ) r ( K r ) θ + ( C r )( K r ) r ) ]=[ 1 r P θ +μ( 1 r r ( r ( K r ) r ) ( K r ) r 2 + 1 r 2 2 ( K r ) θ 2 2 r 2 ( C r ) θ )+ρ×0 ]

[ ρ( t ( K r )+( C r ) r ( K r ) + K r 2 θ ( K r )+ CK r 3 ) ]=[ 1 r P θ +μ( 1 r r ( r r ( K r ) ) K r 3 + 1 r 2 2 θ 2 ( K r ) 2 r 2 θ ( C r ) ) ]

ρ( 0 CK r 3 +0+ CK r 3 )= 1 r P θ +μ( 1 r r ( K r ) K r 3 +00 )

0= 1 r P θ +μ( K r 3 K r 3 +00 )

  1rPθ=0Pθ=0........... (V)

Integrate Equation (V) with respect to θ.

  P(r,θ)=0+g(r)........... (VI)

Here, arbitrary function is g(r).

Differentiate Equation (VI) with respect to r.

  Pr=g(r)........... (VII)

Substitute Cr for ur, 0 for gr and Kr for uθ in Equation (III).

[ ρ( ( C r ) t +( C r ) ( C r ) r + ( K r ) r ( C r ) θ ( K r ) 2 r ) ]=[ P r +μ( 1 r r ( r ( C r ) r ) ( C r ) r 2 + 1 r 2 2 ( C r ) θ 2 2 r 2 ( K r ) θ )+ρ×0 ]

[ ρ( t ( C r )+( C r ) r ( C r ) + K r 2 θ ( C r ) K 2 r 3 ) ]=[ P r +μ( 1 r r ( r r ( C r ) ) C r 3 + 1 r 2 2 θ 2 ( C r ) 2 r 2 θ ( K r ) ) ]

ρ( 0 C 2 r 3 +0 K 2 r 3 )= P r +μ( 1 r r ( C r ) C r 3 +00 )

ρ( C 2 r 3 K 2 r 3 )= P r +μ( C r 3 C r 3 )

  ρ( C 2 r 3 K 2 r 3 )=PrPr=ρ( C 2 + K 2 r 3 )

Substitute ρ(C2+K2r3) for Pr in Equation (VII).

  ρ(C2+K2r3)=g(r)........... (VIII)

Integrate Equation (VIII) with respect to r.

  g(r)=12ρ(C2+K2r2)+C1

Here, arbitrary constant is C1.

Substitute 12ρ(C2+K2r2)+C1 for g(r) in Equation (VI).

  P(r,θ)=12ρ(C2+K2r2)+C1........... (IX)

Conclusion:

The pressure field as a function r and θ is 12ρ(C2+K2r2)+C1.

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Chapter 9 Solutions

Fluid Mechanics: Fundamentals and Applications

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