HWAir flows through a C-d nozzle havinga throat of 0.05m². The Pressure and temperatureat the threat section are 140kPa and 333 K, respectivelyAt Section 2, the pressure is to kla.Find Az and mthroat270 PaAirPt=140kPa7=333K

To analyze the flow through the C-D (converging-diverging) nozzle, we can apply the principles of…

Answered: HW Air flows through a C-d nozzle…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

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HW Air flows through a C-d notcle having a throat of 0.05m². The Pressure and temperature at the threat section are MokPa and 333 K, respectively At Section 2, the pressure is to kla. 2 Find Az and in m 1 Air throat 1270 * Pa Pt=140kPa T=333K
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The jet engine on a test stand, shown in the figure, admitsair at 20oC and 1 atm at section 1, where the area is 0.5 m2and the velocity is 250 m/s. The fuel-to-air ratio is 1:30.The air leaves at section 2 at atmospheric pressure and ahigher temperature. The exit velocity is 900 m/s and thearea is 0.4 m2. Compute the horizontal test stand reactionRx needed to hold the engine fixed.

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HW Air flows through a C-d nozzle having a throat of 0.05m². The Pressure and temperature at the threat section are 140kPa and 333 K, respectively At Section 2, the pressure is to kla. Find Az and m throat 270 Pa Air Pt=140kPa 7=333K