Looking for velocity at the exit and mass flow rate. Show step by step solution please thank youu Current Attempt in ProgressArgon gas flows through a well-insulated nozzle at steady state. The temperature and velocity at the inlet are 550°R and 150 ft/s,respectively. At the exit, the temperature is 440°R and the pressure is 40 Ibf/in?. The area of the exit is 0.0085 ft2. Use the ideal gasmodel with k = 1.67, and neglect potential energy effects.Determine the velocity at the exit, in ft/s, and the mass flow rate, in Ib/s.

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Answered: Argon gas flows through a…

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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Two air flows are mixed to a single flow. One flow is 1.2 kg/s at 25 °C and the other is 2.5kg/s at 220 °C, both at 360 kPa. They combine to generate an exit flow at the same pressure. Find the exit temperature and volume flow rate in (L/s). ro
You have a tank that is 0.01 m^3 and is initially evacuated. You then hook this up to a line that supplies N2 at a pressure of P_1 = 5 bar and a T_1 = 350 K. The tank fills adiabatically (you can assume there is no heat flow to the walls of the tank), and the filling ends when no more N2 flows into the tank. Find a) the final pressure of the gas in the tank, and b) the final temperature of the gas in the tank. You can assume N2 is an ideal gas with a CP* = 29 J/mol K. NOTE: Mainly I am confused on how the evacuated tank factors into the work for b). What I did was use the ideal gas formula to find a value for N2*T2 (601.395) but I am no longer certain how to continue in the work. I was assuming the practice question had meant the temperature of the tank was 0 initially but it leads to a negative mole value. For a) I got 5 bar, arguing the flow would stop when the pressure of tank and line are equal
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