A flow with Mach number M1 = 2 and pressure p1 = 1 atm is turned away from itself twice, first through an angle of 10 deg and then through a second angle of 20 deg. Compute the Mach number and the static pressure downstream of the second turn. Then, suppose that the original flow (M1 = 2 and p1 = 1 atm) is turned away from itself through a single turn of 30 deg. Compute the Mach number and static pressure downstream of this turn, and show that the values are the same as for the first flow with two turns totaling 30 deg.
A flow with Mach number M1 = 2 and pressure p1 = 1 atm is turned away from itself twice, first through an angle of 10 deg and then through a second angle of 20 deg. Compute the Mach number and the static pressure downstream of the second turn. Then, suppose that the original flow (M1 = 2 and p1 = 1 atm) is turned away from itself through a single turn of 30 deg. Compute the Mach number and static pressure downstream of this turn, and show that the values are the same as for the first flow with two turns totaling 30 deg.
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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A flow with Mach number M1 = 2 and pressure p1 = 1 atm is turned away from itself twice,
first through an angle of 10 deg and then through a second angle of 20 deg. Compute the Mach
number and the static pressure downstream of the second turn. Then, suppose that the original flow
(M1 = 2 and p1 = 1 atm) is turned away from itself through a single turn of 30 deg. Compute the
Mach number and static pressure downstream of this turn, and show that the values are the same
as for the first flow with two turns totaling 30 deg.
3
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