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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Textbook Question
Chapter 12, Problem 64P
Air flows isentropically through a converging nozzle into a receiver where the pressure is 250 kPa absolute. If the pressure is 350 kPa absolute and the speed is 150 m/s at the nozzle location where the Mach number is 0.5, determine the pressure, speed, and Mach number at the nozzle throat.
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Air is flowing in the converging-diverging nozzle shown in the figure below.
A = 15 cm²
A₁ = 10 cm²
Determine the three critical pressure ratios.
"pc1= i
"pc2= i
*pc3 =
Shock
i
A = 25 cm²
Determine the Mach number immediately upstream from the shock.
Ma₁ = i
Determine the Mach number immediately downstream from the shock.
Ma₂ i
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Chapter 12 Solutions
Fox And Mcdonald's Introduction To Fluid Mechanics
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