The back pressure if the flow were isentropic throughout is ....... Air at stagnation pressure of 600 kpa and stagnation temperature of 530 K enters a frictionless convergent-divergent nozzle as shown in figure the throat area is 5cm² and the exit area is 12.5 cm², the back pressure is 300kpa, and normal shock occurs within the divergent section. Determine the following: 2 Po 700 kPa i To-530 K A₁-5 cm² P-350 kPa A₂ = 12,5 cm²

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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The back pressure if the flow were
isentropic throughout is
Air at stagnation pressure of 600 kpa and stagnation temperature of 530 K enters a frictionless
convergent-divergent nozzle as shown in figure the throat area is 5cm² and the exit area is
12.5 cm², the back pressure is 300kpa, and normal shock occurs within the
divergent section. Determine the following:
2
Po 700 kPa i
To 530 K
A₁-5 cm²
y
-
P-350 kPa
A₂ = 12.5 cm²
Transcribed Image Text:The back pressure if the flow were isentropic throughout is Air at stagnation pressure of 600 kpa and stagnation temperature of 530 K enters a frictionless convergent-divergent nozzle as shown in figure the throat area is 5cm² and the exit area is 12.5 cm², the back pressure is 300kpa, and normal shock occurs within the divergent section. Determine the following: 2 Po 700 kPa i To 530 K A₁-5 cm² y - P-350 kPa A₂ = 12.5 cm²
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