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For isentropic air flow through a cd nozzle shown in figure, the stagnation conditions are To=300 K and P. = I bar, the throat area is 0.1 m² and the exit area is 0.2 m². If the Mach number at throat is 0.6, calculate the velocity and the density of the air at the exit. Po 1 bar TB-300 K Throat M₁ = 0.6 exit A₁-0.1 m² A-0.2 m²

For isentropic air flow through a cd nozzle shown in figure, the stagnation conditions are To=300 K and P. = I bar, the throat area is 0.1 m² and the exit area is 0.2 m². If the Mach number at throat is 0.6, calculate the velocity and the density of the air at the exit. Po 1 bar TB-300 K Throat M₁ = 0.6 exit A₁-0.1 m² A-0.2 m²

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
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For isentropic air flow through a cd nozzle shown in figure, the stagnation conditions are To=300 K and P. = I bar, the throat area is 0.1 m² and the exit area is 0.2 m². If the Mach number at throat is 0.6, calculate the velocity and the density of the air at the exit. Po 1 bar TB-300 K Throat M₁ = 0.6 exit A₁-0.1 m² A-0.2 m²
Transcribed Image Text:For isentropic air flow through a cd nozzle shown in figure, the stagnation conditions are To=300 K and P. = I bar, the throat area is 0.1 m² and the exit area is 0.2 m². If the Mach number at throat is 0.6, calculate the velocity and the density of the air at the exit. Po 1 bar TB-300 K Throat M₁ = 0.6 exit A₁-0.1 m² A-0.2 m²
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