An aircraft with nose M1 P1 T1 properties of the upstream unifrom air M2 angle 0 = 15° as shown in figure, flies with Mach number M1 %3D = 2.5. The %3D are P1 = 60 kPa, and T = 265 K. Find: %3D
An aircraft with nose M1 P1 T1 properties of the upstream unifrom air M2 angle 0 = 15° as shown in figure, flies with Mach number M1 %3D = 2.5. The %3D are P1 = 60 kPa, and T = 265 K. Find: %3D
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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Question
The angle of the weak oblique shock wave =
The angle of the strong oblique shock wave =
Mach number downstream the weak oblique shock wave (M2)
Pressure downstream the weak oblique shock wave
Temperature downstream the weak oblique shock wave

Transcribed Image Text:An aircraft with nose
M1
angle e = 15° as shown in figure, flies
P1
= 2.5. The
T1
properties of the upstream unifrom air
with Mach number M1
are P1 60 kPa, and T = 265 K. Find:
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