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 8, Problem 152P
To determine

The coefficient of discharge of the orifice.

Expert Solution & Answer
Check Mark

Answer to Problem 152P

The coefficient of discharge is 0.237.

Explanation of Solution

Given information:

The diameter of tank 1 is 30cm, diameter of tank 2 is 12cm, diameter of orifice is 5mm. The fluid height in tank 1 is 45cm and the fluid height in tank 2 is 15cm. The time taken to stop the flow is 200s. The loss of head due to friction is negligible.

Assume the free surface for tank as 1 and the exit of orifice as 0.

Write the expression to calculate the energy equation for the system.

  P1ρg+α1V122g+z1+hpump=P0ρg+α0V022g+z0+hturbine+hL  ......(I)

Here, the pressure in tank is P1, datum head in tank is z1, the pressure in orifice is P0, datum head in orifice is z0, the kinetic energy correction factor for tank 1 is α1, the kinetic energy correction factor for orifice is α0, the turbine head is hturbine, the pump head is hpump, the head loss due to the friction is hL, the density is ρ and the gravitational acceleration is g.

The surface of the tank is open to atmosphere.

  P1=Patm

Here, the atmospheric pressure is Patm.

Write the expression for the pressure in orifice.

  P0=Patm+ρgh2

Here, the fluid height in tank 2 is h2.

Write the expression for the net fluid height in the system.

  h=h1h2  ......(II)

Here, the height in tank 1 is h1.

Write the Equation (II) in derivative form.

  dh=dh1dh2dh2=dh1dh

Here, the fluid height in tank is h1.

Write the expression for the volume flow rate through the orifice.

  V˙=CdV0A0   ...... (III)

Here, the coefficient of discharge is Cd, the area of orifice is A0 and the velocity at the exit of the orifice is V0.

Write the expression for the volume flow through orifice in terms of time derivatives.

  V˙=A2dh2dtV˙=A1dh1dtA1dh1dt=A2dh2dtdh2=A1A2dh1  ......(IV)

Here, the area of tank 2 is A2 and the area of tank 1 is A1.

Write the expression for the area of tank 1.

  A1=π4D12

Here, the diameter of tank 1 is D1.

Write the expression for the area of tank 2.

  A2=π4D22

Here, the diameter of tank 2is D2.

Write the expression for the area of orifice.

  A0=π4D02

Here, the diameter of orifice is D0.

Calculation:

Substitute 0 for V1, Patm for P1, h1 for z1, 0 for hturbine, 0 for hpump, 0 for hL, Patm+ρgh2 for P0, 0 for z2, 1 for α1 and 1 for α0 in Equation (I).

  Patmρg+(1)(0)22g+h1+0=Patm+ρgh2ρg(1)V022g+0+0+0h1=ρgh2ρg+V022gh1=h2+V022gV0=2g(h1h2)   ....... (V)

Substitute h for (h1h2) in Equation (V).

  V0=2gh   ....... (VI)

Substitute dh1dh for dh2 in Equation (IV).

  dh1dh=A1A2dh1dh=dh1(1+A1A2)dh1=dh(1+ A 1 A 2 )

Substitute A1dh1dt for V˙ in Equation (III).

  A1dh1dt=CdV0A0dt=A1(dh1CdV0A0)   ....... (VII)

Substitute dh(1+A1A2) for dh1 and 2gh for V0 in Equation (VII).

  dt=A1(( dh ( 1+ A1 A2 ) )Cd( 2gh )A0)dt=A1(dhCd( 1+ A1 A2 )( 2gh )A0)dt=A1A2dhCdA0(A1+A2)( 2gh)   ...... (VIII)

Integrate Equation (VIII) with limits 0 to t in left- hand side and limits z1 to z in right-hand side.

  0tdt=h1hA1A2dhCdA0( A 1+ A 2)( 2gh)(t)0t=A1A2CdA0(A1+A2)(2g)(h 1 212)h1h(t0)=A1A2CdA0(A1+A2)(2g)(h1212h11212)Cd=2A1A2A0(A1+A2)(t)(2g)(h12h112)   ....... (IX)

Substitute π4D02 for A0, π4D12 for A1, and π4D22 for A2 in Equation (IX).

  Cd=2(π4D12)(π4D22)(π4D02)(π4D12+π4D22)(t)( 2g)(h12h112)Cd=2(D12)(D22)(D02)(D12+D22)(t)( 2g)(h112h12)   ....... (X)

Substitute 45cm for h1, 0 for h, 30cm for D1, 5mm for D0, 12cm for D2, 9.81m/s2 for g, 200s for t in Equation (X).

   C d =( 2 ( 30cm ) 2 ( 12cm ) 2 ( ( 5mm ) 2 )( ( 30cm ) 2 + ( 12cm ) 2 )( 200s )( 2( 9.81m/ s 2 ) ) ×( ( 45cm ) 1 2 ( 0 ) 1 2 ) )

   =( 2 ( 30cm( 1m 100cm ) ) 2 ( 12cm( 1m 100cm ) ) 2 ( ( 5mm( 1m 1000mm ) ) 2 )( ( 30cm( 1m 100cm ) ) 2 + ( 12cm( 1m 100cm ) ) 2 )( 200s )( 2( 9.81m/ s 2 ) ) ×( ( 45cm( 1m 100cm ) ) 1 2 ( 0 ) 1 2 ) )

   =0.237

Conclusion:

The coefficient of discharge is 0.237.

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Chapter 8 Solutions

Fluid Mechanics: Fundamentals and Applications

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