In choked flow and in supersonic flow the standing shock wave prevents downstream equipment from communicating back to the source (e.g., friction in downstream pipe is not a factor in the mass flow rate). In subsonic flow, the downstream effects are able to communicate back to the source and downstream effects do change mass flow rate.
This effect is vividly evident in a diverging nozzle:
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[li]For incompressible flow (i.e., velocity below about 0.6 M), an increase in cross sectional area causes a decrease in velocity at an increasing pressure.[/li]
[li]For compressible flow an increase in cross sectional area causes the shock wave to expand and allow an increase in velocity at a constant pressure.[/li]
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Mathematically, mass flow rate is volume flow rate times density. Volume flow rate is a function of area and velocity (assuming the discharge coefficient is constant):
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[li]Above about Mach 0.6, velocity is a function of temperature, without a pressure component. Density is a function of both temperature and pressure, so at a constant temperature, mass flow rate is a linear function of pressure.[/li]
[li]At lower velocities, the velocity is a function of the volume flow rate at actual conditions which has a term that is the difference of the square of the upstream pressure minus the square of the downstream pressure. With everything except upstream pressure held constant (the friction factor is not constant, but is pretty close for small changes in upstream pressure) then the mass flow rate term will approximate a parabola (but will deviate because of subtracting the downstream pressure and the changes in the friction factor).[/li]
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David Simpson, PE
MuleShoe Engineering
In questions of science, the authority of a thousand is not worth the humble reasoning of a single individual. Galileo Galilei, Italian Physicist