Fox And Mcdonald's Introduction To Fluid Mechanics
Fox And Mcdonald's Introduction To Fluid Mechanics
9th Edition
ISBN: 9781118921876
Author: Pritchard, Philip J.; Leylegian, John C.; Bhaskaran, Rajesh
Publisher: WILEY
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Chapter 1, Problem 27P

The maximum theoretical flow rate (slug/s) through a supersonic nozzle is

m ˙ max = 2.38 A t p 0 T 0

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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Chapter 1 Solutions

Fox And Mcdonald's Introduction To Fluid Mechanics

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