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5. 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 back pressure if the flow were isentropic throughout Оa- 38kpa Ob- 48kpa Ос- 58kpa Od- 68kpa

5. 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 back pressure if the flow were isentropic throughout Оa- 38kpa Ob- 48kpa Ос- 58kpa Od- 68kpa

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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5. 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 back pressure if the flow were isentropic throughout Оa- 38kpa Ob- 48kpa Ос- 58kpa Od- 68kpa
Transcribed Image Text:5. 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 back pressure if the flow were isentropic throughout Оa- 38kpa Ob- 48kpa Ос- 58kpa Od- 68kpa
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