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3.4. Consider a normal shock wave in air The upstream conditions are given by M 3; 1 atm, and p, = 1 23 kg/m' Calculate the downstream values of P2, T, Pu M2, u2, Po,, and 7, P1 02

3.4. Consider a normal shock wave in air The upstream conditions are given by M 3; 1 atm, and p, = 1 23 kg/m' Calculate the downstream values of P2, T, Pu M2, u2, Po,, and 7, P1 02

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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are 3000 ft/s and 500°R, respectively Calculate the Mach number M and the characteristic Mach number M* at this point 3.4. Consider a normal shock wave in air The upstream conditions are given by M = 3; P1 M2, u2, Po,, and T %3! = 1 atm, and p, = 1 23 kg/m Calculate the downstream values of P2, 02 35 Consider a Pitot static tube mounted on the pose of an experımental airplane A
Transcribed Image Text:are 3000 ft/s and 500°R, respectively Calculate the Mach number M and the characteristic Mach number M* at this point 3.4. Consider a normal shock wave in air The upstream conditions are given by M = 3; P1 M2, u2, Po,, and T %3! = 1 atm, and p, = 1 23 kg/m Calculate the downstream values of P2, 02 35 Consider a Pitot static tube mounted on the pose of an experımental airplane A
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