The maximum theoretical flow rate (slug/s) through a supersonic nozzle is
where At(ft2) is the nozzle throat area, p0 (psia) is the tank pressure, and T0(R) is the tank temperature. Is this equation dimensionally correct? If not, find the units of the 2.38 term. Write the equivalent equation in SI units.
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Fox and McDonald's Introduction to Fluid Mechanics
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