What Does the Graph in My Compressive Flow Experiment Indicate?

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The discussion centers on interpreting a graph depicting pressure variations in a converging-diverging nozzle under different supply and back pressures. The user seeks clarification on where the graph indicates sonic speeds, particularly at the nozzle throat where fluid cannot exceed Mach 1. Additionally, it is noted that as the pressure difference increases, the P/Po ratio approaches the critical pressure ratio of 0.5283 for air. The user is looking for insights to complete their homework by Friday. Understanding these relationships is crucial for analyzing compressive flow behavior in nozzles.
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Homework Statement


Wondering if anyone could give me a hand, I have created the attached graph. It shows the variations of pressure in the nozzle for different supply pressures and back pressures, in the form, P/Po vs position of the nozzle. and not too sure what its showing


Homework Equations


Wondering if anyone can help me figure out what the graph is showing??


The Attempt at a Solution


Picture1.png
 
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I didn't mention that the nozzle a converging- diverging nozzle. Also I know that at the throat of the nozzle the fluid cannot reach speeds above Mach 1, sonic speeds. However i am wondering where on the graph this relates too.\

I also know that the Pc/Po(critical pressure ratio) for air is 0.5283 and it seems that as the pressure difference becomes larger the closer the P/Po becomes to the critical ratio value.

Any help will be greatly appreciated as this has to be submitted by friday.

Thanks
John
 
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