An industrial nozzle as shown in Figure 3 works with an inert gas rush through the nozzle where the speed of the gas at the nozzle throat is recorded equal to the speed of sound. The inlet velocity, temperature, and pressure are 98 m/s, 600 oC, and 88 psi, respectively. Take the property of inert gas for k = 1.66 and cp = 5.192 kJ/kg. K. Calculate: a) Stagnation pressure b) Mach number at the nozzle inlet c) Temperature of the gas at the throat d) Pressure of the gas at the throat
An industrial nozzle as shown in Figure 3 works with an inert gas rush through the nozzle where the speed of the gas at the nozzle throat is recorded equal to the speed of sound. The inlet velocity, temperature, and pressure are 98 m/s, 600 oC, and 88 psi, respectively. Take the property of inert gas for k = 1.66 and cp = 5.192 kJ/kg. K. Calculate: a) Stagnation pressure b) Mach number at the nozzle inlet c) Temperature of the gas at the throat d) Pressure of the gas at the throat
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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An industrial nozzle as shown in Figure 3 works with an inert gas rush through the nozzle where the speed of the gas at the nozzle throat is recorded equal to the speed of sound. The inlet velocity, temperature, and pressure are 98 m/s, 600 oC, and 88 psi, respectively.
Take the property of inert gas for k = 1.66 and cp = 5.192 kJ/kg. K. Calculate:
a) Stagnation pressure
b) Mach number at the nozzle inlet
c) Temperature of the gas at the throat
d) Pressure of the gas at the throat
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