Finding Input to Output Ratio for Steady Water Flow

AI Thread Summary
To maintain steady water flow through a nozzle, the input and output diameters must be proportionate based on the flow speeds and pressures. The input flow speed is 3.00 m/s at a pressure of 1.31 x 10^5 Pa, while the output speed is calculated to be 5.58 m/s using Bernoulli's equation. The area ratio of the input to output can be derived from the relationship A1v1 = A2v2, resulting in a ratio of approximately 0.5376. It is confirmed that the external pressure is atmospheric pressure, which is essential for the calculations. Understanding these principles is crucial for solving fluid dynamics problems effectively.
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


<br /> P_{{\rm{input}}} + \frac{{\rho v_{{\rm{input}}}^2 }}{2} = P_{{\rm{atmosphere}}} + \frac{{\rho v_{{\rm{output}}}^{\rm{2}} }}{2}<br />

A_1 v_1 = A_2 v_2

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?
<br /> \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}<br />

\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}
 
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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

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

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