An analysis of the head lost in a nozzle and the resulting velocity of the jet.

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Introduction

Assumptions

It is assumed that the Head H is the head behind the nozzle and that all pipeline and valve losses have been accounted for elsewhere. There are, of course, losses in the nozzle itself and the actual velocity of discharge will be less than the theoretical value by one to five percent. This is catered for by the use of The Coefficient of Velocity C_V, The Coefficient of Contraction C_C and the Coefficient of Discharge C_D:

  • C_V = Actual Velocity / Theoretical Velocity
  • C_C = Actual cross sectional area / Geometric cross sectional Area
  • C_D = C_C\times C_V

The head Lost in the Nozzle

22109/img_0001_6.png

Let H = total head at nozzle (i.e. the sum of the pressure and velocity heads)

H=H_1- L
(1)

where L represents the Pipe line losses

V^2 = {C_{V}}^{2}\;2\,g\,H
(2)

H = \displaystyle\frac{V^2}{{C_{V}}^{2}\;2\,g}

Head behind the Nozzle = Head after the nozzle + Head lost in Nozzle H = \frac{v^2}{2g} + H_l where H_l represents the head lost

Substituting from (#2) above:

\therefore\:H_l = H-C_{v}^{2}\:H
(3)

Therefore, the head lost in nozzle is H_l= H (1 - {C_{v}}^{2}) or H_l = H(1 - {C_{V}}^{2}) = \displaystyle\frac{V^2}{{C_{V}}^{2}\times2\,g}\left (1 - {C_{V}}^{2} \right ) \therefore \;\;\;\;\;\;\;H_l = \frac{V^2}{2\,g}\left (\frac{1}{{C_{V}}^{2}} - 1 \right )

Efficiency of the Nozzle

Efficiency in general describes the extent to which time or effort is well used for the intended task or purpose. It may be defined as

\eta = \displaystyle\frac{\dfrac{v^2}{2g}}{H}
(4)

where H represents the Head behind the nozzle i.e. \eta= \frac{v^2}{2g\:H} =\frac{C_v\; \sqrt{2g\:H}}{2g\,H} = C_v^2 Thus, C_V=\sqrt{\eta}

The Power of a Jet

Power is the rate at which work is done, expressed as the amount of work per unit time and commonly measured in units such as the watt and horsepower.

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Let the weight of fluid discharged be W. Then if the effective cross sectional are of the jet is a and the velocity of discharge is V then the Kinetic Energy of the Jet is: \frac{1}{2} \displaystyle\frac{W}{g} V^2 =\frac{1}{2}\times \frac{w\,a\,V}{2\,g}\timesV^2 = \frac{w\,a\,V^3}{2\,g}

For the Jet the Work Done equals the change of Kinetic Energy and hence the power available in the jet is \frac{w\,a\,V^3}{2\,g\times 550}

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