Q3. A supersonic flow of air has a pressure of 1 x 105 N/m2 andMa temperature of 350 K. After expanding through a 35° turm,the Mach number is 3.5. Determine:Angles 8,,02 and 03.0= ?Final flow properties p2 and T2.Figure Q3

given data;⇒pressure(P)=1*105N/m2⇒temperature(T)=350K⇒mack number(M)=3.5

Answered: Q3. A supersonic flow of air has a…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

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Q3. A supersonic flow of air has a pressure of 1 x 105 N/m2 and My a temperature of 350 K. After expanding through a 35° tum, the Mach number is 3.5. Determine: • Angles 0,,02 and 63. Final flow properties p2 and T2. Figure Q3