Finding Input to Output Ratio for Steady Water Flow

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SUMMARY

The discussion focuses on calculating the input to output diameter ratio for steady water flow through a nozzle, given an input speed of 3.00 m/s and an input pressure of 1.31 x 105 Pa. Using Bernoulli's equation and the continuity equation, the output speed is determined to be 5.58 m/s. Consequently, the input to output area ratio is calculated as 0.5376, indicating that the output diameter must be smaller than the input diameter to maintain steady flow.

PREREQUISITES
  • Understanding of Bernoulli's equation
  • Familiarity with the continuity equation in fluid dynamics
  • Knowledge of pressure units (Pa) and fluid density (kg/m3)
  • Basic algebra for solving equations
NEXT STEPS
  • Study Bernoulli's equation applications in fluid dynamics
  • Learn about the continuity equation and its implications for flow rates
  • Explore the effects of varying fluid densities on flow behavior
  • Investigate nozzle design principles for optimizing flow efficiency
USEFUL FOR

Students in fluid mechanics, engineers designing fluid systems, and anyone involved in hydraulic analysis or nozzle design will benefit from this discussion.

tony873004
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Homework Statement


Water flows into a nozzle at 3.00 m/s at a pressure of 1.31*105Pa. What should the ratio of input to output diameter be if the flow is to remain steady? What is the flow speed at the exit?


Homework Equations


[tex] P_{{\rm{input}}} + \frac{{\rho v_{{\rm{input}}}^2 }}{2} = P_{{\rm{atmosphere}}} + \frac{{\rho v_{{\rm{output}}}^{\rm{2}} }}{2}[/tex]

[tex]A_1 v_1 = A_2 v_2[/tex]

The Attempt at a Solution


My first guess is to simply say that a 1:1 input:output ratio with the water flowing out at the same speed as it flows in should do the trick. But that would be too easy. I guess that I'm to assume that the pressure outside is air pressure. If so, am I doing it right?
[tex] \begin{array}{l}<br /> P_{{\rm{input}}} + \frac{{\rho v_{{\rm{input}}}^2 }}{2} = P_{{\rm{atmosphere}}} + \frac{{\rho v_{{\rm{output}}}^{\rm{2}} }}{2} \\ <br /> \\ <br /> P_{{\rm{input}}} + \frac{{\rho v_{{\rm{input}}}^2 }}{2} - P_{{\rm{atmosphere}}} = \frac{{\rho v_{{\rm{output}}}^{\rm{2}} }}{2} \\ <br /> \\ <br /> \frac{{2\left( {P_{{\rm{input}}} + \frac{{\rho v_{{\rm{input}}}^2 }}{2} - P_{{\rm{atmosphere}}} } \right)}}{\rho } = v_{{\rm{output}}}^{\rm{2}} \\ <br /> \\ <br /> v_{{\rm{output}}}^{} = \sqrt {\frac{{2\left( {P_{{\rm{input}}} + \frac{{\rho v_{{\rm{input}}}^2 }}{2} - P_{{\rm{atmosphere}}} } \right)}}{\rho }} \\ <br /> \\ <br /> v_{{\rm{output}}}^{} = \sqrt {\frac{{2\left( {1.31 \times 10^5 \,{\rm{Pa}} + \frac{{\left( {1000\frac{{{\rm{kg}}}}{{{\rm{m}}^{\rm{3}} }}} \right)\left( {3.00\,{\rm{m/s}}^{\rm{2}} } \right)}}{2} - 101.325 \times 10^3 \,{\rm{Pa}}} \right)}}{{\left( {1000\frac{{{\rm{kg}}}}{{{\rm{m}}^{\rm{3}} }}} \right)}}} = 5.58{\rm{ m/s}} \\ <br /> \end{array}[/tex]

[tex]\begin{array}{l}<br /> A_1 v_1 = A_2 v_2 \\ <br /> \\ <br /> \frac{{A_1 }}{{A_2 }} = \frac{{v_2 }}{{v_1 }} = \frac{{3.00\;{\rm{m/s}}}}{{{\rm{5}}{\rm{.58}}\,{\rm{m/s}}}} = 0.5376 \\ <br /> \end{array}[/tex]
 
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tony873004 said:
Water flows into a nozzle at 3.00 m/s at a pressure of 1.31*105Pa. What should the ratio of input to output diameter be if the flow is to remain steady? What is the flow speed at the exit?

My first guess is to simply say that a 1:1 input:output ratio with the water flowing out at the same speed as it flows in should do the trick. But that would be too easy. I guess that I'm to assume that the pressure outside is air pressure. If so, am I doing it right?

Hi tony! :smile:

Yes … air pressure …

but it would be simpler just to say

[tex]\Delta(v^2) = \left(\frac{2}{\rho}\right)\,\Delta P[/tex]

[tex]v_1 = \sqrt{v_0^2\ +\ \left(\frac{2}{\rho}\right)\,\Delta P\ }[/tex] :smile:
 

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