Air flows isentropically through a duct. At section 1, the pressure and temperature are 250 kPaand 200°C, respectively and the velocity is 250 m/s. At section 2, the area is 0.25 m² and theMach number is 2.0. Determine (a) Ma₁, (b) T2, (c) V2, and (d) the mass flow.

Isentropic Flow AnalysisAir flows isentropically through a duct. At section 1, the pressure and…

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Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

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It is a Thermodynamics subject please show the complete and step by step solution. Use the given format I inserted. Please answer it as soon as possible.
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4)Carbon dioxide flows steadily through a varying cross-sectional-area duct such as a nozzle shown in the figure. The throat area is (10+0.1*A) cm². The carbon dioxide enters the duct at a pressure of (1400+A) kPa and 200°C with a low velocity, and it expands in the nozzle to a pressure of 200 kPa. The duct is designed so that the flow can be approximated as isentropic. Determine the flow rate in the nozzle. A = LAST DIGIT OF YOUR CLASS ID Stagnation region 1400 - ALPw 200°C CO₂ 1400 P. KP
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Air flows isentropically through a duct. At section 1, the pressure and temperature are 250 kPa and 200°C, respectively and the velocity is 250 m/s. At section 2, the area is 0.25 m² and the Mach number is 2.0. Determine (a) Ma₁, (b) T2, (c) V2, and (d) the mass flow.