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Q1: A convergent-divergent nozzle has an exit area to throat area ratio of underline 2 Air enters the nozzles with a stagnation pressure of 6.5 bar and a stagnation temperature of 93 degrees * C The throa area is 6.25 cm ^2 If there is a normal shock wave standing at a point where M= 1.5, determine the oither eide of the pla ne of pre 0O

Q1: A convergent-divergent nozzle has an exit area to throat area ratio of underline 2 Air enters the nozzles with a stagnation pressure of 6.5 bar and a stagnation temperature of 93 degrees * C The throa area is 6.25 cm ^2 If there is a normal shock wave standing at a point where M= 1.5, determine the oither eide of the pla ne of pre 0O

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
Problem 1.1MA
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Q1: A convergent-divergent nozzle has an exit area to throat area ratio of underline 2 Air enters the nozzles with a stagnation pressure of 6.5 bar and a stagnation temperature of 93 degrees * C The throat area is 6.25 cm ^ 2 If there is a normal shock wave standing at a point where M= 1.5, determine the pressure, temperature on either side of the plane of shock and the mach number on the downstream side of the plane. Find also the exit mach number of the nozzle. p 2:44 /
Transcribed Image Text:Q1: A convergent-divergent nozzle has an exit area to throat area ratio of underline 2 Air enters the nozzles with a stagnation pressure of 6.5 bar and a stagnation temperature of 93 degrees * C The throat area is 6.25 cm ^ 2 If there is a normal shock wave standing at a point where M= 1.5, determine the pressure, temperature on either side of the plane of shock and the mach number on the downstream side of the plane. Find also the exit mach number of the nozzle. p 2:44 /
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