The converging-diverging nozzle(as shown in the figure given below) expands and accelerates dry air to supersonicspeeds at the exit where p2 = 8 kPa and T₂ = 240 K. At the throat, p₁ = 284 kPa, T₁= 665 K, and V₁ = 495 m/s.NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part.Air-D₁ = 1 cmKg/sD₂ = 2.5 cmDetermine the mass flow for a steady compressible flow of an ideal gas.

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Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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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 p2 = 8 kPa and T₂ = 240 K. At the throat, p₁ = 284 kPa, T₁= 665 K, and V₁ = 495 m/s.
NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part.
Air-
D₁ = 1 cm
Kg/s
D₂ = 2.5 cm
Determine the mass flow for a steady compressible flow of an ideal gas.

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Step 1

$g i v e n d a t a a t n o z z l e i n l e t d i a m e t e r (D_{1}) = 1 c m i n l e t p r e s s u r e (P_{1}) = 284 k p a i n l e t t e m p e r a t u r e (T_{1}) = 665 k p a i n l e t v e l o c i t y (V_{1}) = 495 m / s o u t l e t d i a m e t e r (D_{2} = 2.5 c m o u t l e t p r e s s u r e (P_{2}) = 8 k p a o u t l e t t e m p e r a t u r e (T_{2}) = 240 k w e h a v e t o d e t e r m i n e t h e m a s s f l o w f o r s t e a d y f l o w$

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