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50 Ma, = 1 i 0 = 0, max 40 30 Maj→ 00 Maz > 1 Ma, < 1 20 Weak Strong 10 10 /5 3. 1.5 1.2 10 20 30 50 60 70 80 90 ß, degrees 0, degrees

50 Ma, = 1 i 0 = 0, max 40 30 Maj→ 00 Maz > 1 Ma, < 1 20 Weak Strong 10 10 /5 3. 1.5 1.2 10 20 30 50 60 70 80 90 ß, degrees 0, degrees

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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Consider supersonic airflow approaching the nose of a two-dimensional wedge at a Mach number of 3. Using Fig. , determine the minimum shock angle and the maximum deflection angle a straight oblique shock can have.

50 Ma, = 1 i 0 = 0, max 40 30 Maj→ 00 Maz > 1 Ma, < 1 20 Weak Strong 10 10 /5 3. 1.5 1.2 10 20 30 50 60 70 80 90 ß, degrees 0, degrees
Transcribed Image Text:50 Ma, = 1 i 0 = 0, max 40 30 Maj→ 00 Maz > 1 Ma, < 1 20 Weak Strong 10 10 /5 3. 1.5 1.2 10 20 30 50 60 70 80 90 ß, degrees 0, degrees
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