The converging-diverging nozzle(as shown in the figure given below) expands and accelerates dry air to supersonic speeds at the exit where $P_{2} = 8 kPa$ and $T_{2} = 240 K$ . At the throat, $P_{1} = 284 kPa, T_{1} = 665 K$ , and $V_{1} = 495 m / s$ . NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Determine the mass flow for a steady compressible flow of an ideal gas. $Kg / s$

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The converging-diverging nozzle(as shown in the figure given below) expands and accelerates dry air to supersonic speeds at the exit where

P_{2} = 8 kPa

and

T_{2} = 240 K

. At the throat,

P_{1} = 284 kPa, T_{1} = 665 K

, and

V_{1} = 495 m / s

. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Determine the mass flow for a steady compressible flow of an ideal gas.

Kg / s

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