Need proper answer with details explanation (b) The McDonnell Dauglas F-15 Eagle has a convergent -divergent duct exhaust system.Assuming the exhaust product as air and flowing isentropically through the duct as shownin Fig. for Q.7(b). Compute To, Mar, Po, A* and m. If the area at section 2 is 0.036 m²,Compute Maand P₂if the flow is subsonic or supersonic. Take k=1.4.SubsonicA₁ = 0.05m₁ =180 m/sP₁ = 500 kT₁ = 470K.20Throat2F2fiPossiblySupersonicA₂ = 0.036 m²Fig-for & 7(b)

To find:the temperature, the Mach number, pressure, area, and mass flow rate at the inlet.and at…

5) The McDonnell Dauglas F-15 Eagle has a convergent -divergent duct exhaust system. Assuming the exhaust product as air and flowing isentropically through the duct as shown in Fig. for Q.7(b). Compute To, Ma, Po, A* and m. If the area at section 2 is 0.036 m², Compute Maand P₂ if the flow is subsonic or supersonic. Take k-1.4. A₁ = 0.05 m ₁ = 180 m/s P₁= 500 k T₁ = 470 K. Subsonic I 2 Throat 2F Possibly Supersonic A₂ = 0.036 m Fig-for & 7 (b)

5) The McDonnell Dauglas F-15 Eagle has a convergent -divergent duct exhaust system. Assuming the exhaust product as air and flowing isentropically through the duct as shown in Fig. for Q.7(b). Compute To, Ma, Po, A* and m. If the area at section 2 is 0.036 m², Compute Maand P₂ if the flow is subsonic or supersonic. Take k-1.4. A₁ = 0.05 m ₁ = 180 m/s P₁= 500 k T₁ = 470 K. Subsonic I 2 Throat 2F Possibly Supersonic A₂ = 0.036 m Fig-for & 7 (b)

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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