Upstream of the throat of an isentropic converging-diverging nozzle at section (1), V₁ = 150 m/s,P1 = 100 kPa (abs), T₁ = 20°C. If the discharge flow is supersonic and the throat area is 0.10 m²,determine the mass flowrate in kg/s for the flow of air.kg/sm = i

The velocity at the inlet throat is the pressure is The temperature is the area of the throat is

Upstream of the throat of an isentropic converging-diverging nozzle at section (1), V₁ = 150 m/s, P₁ = 100 kPa (abs), T₁= 20°C. If the discharge flow is supersonic and the throat area is 0.10 m², determine the mass flowrate in kg/s for the flow of air. kg/s m = i

Upstream of the throat of an isentropic converging-diverging nozzle at section (1), V₁ = 150 m/s, P₁ = 100 kPa (abs), T₁= 20°C. If the discharge flow is supersonic and the throat area is 0.10 m², determine the mass flowrate in kg/s for the flow of air. kg/s m = i

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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Question

Upstream of the throat of an isentropic converging-diverging nozzle at section (1), V₁ = 150 m/s,
P1 = 100 kPa (abs), T₁ = 20°C. If the discharge flow is supersonic and the throat area is 0.10 m²,
determine the mass flowrate in kg/s for the flow of air.
kg/s
m = i

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