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.

ChapterMA: Math Assessment

Section: Chapter Questions

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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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If 8.5kg of of air are compressed isothermally from 90kPa 8m3 to 600kPa. Find the change in entropy (kJ/K)
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At the inlet to a certain nozzle the enthalpy of fluid passing is 2800 kJ/Kg. In addition, the velocity is 50 m/s. At the discharge end, the enthalpy is 2600 kJkg. The nozzle is horizontal and there is negligible heat loss from it. a. Find the velocity at the exit of the nozzle? b. If the inlet area is 900 cm and specific vohme at the inlet is 0.187 m'kg, find the mass flowrate? c. If the specific volume at the exit of the nozzle is 0.498 m/kg, find the exit area of nozzle? Fhuid in Fhaid out V2= ? A2= ? V- 50 m/s A- 900 cm? hi- 2800 kJ/kg h2= 2600 kJ/kg
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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