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Category > Engineering Posted 15 May 2017 My Price 12.00

A converging–diverging nozzle operating at steady state has

(CD-ROM)

For the nozzle in Problem 12.59, determine the back pressure, in bar, for which a normal shock would stand at the exit plane.

Problem 12.59:

A converging–diverging nozzle operating at steady state has a throat area of 3 cm2 and an exit area of 6 cm2 . Air as an ideal gas with k = 1.4 enters the nozzle at 8 bar, 400 K, and a Mach number of 0.2, and flows isentropically throughout. If the nozzle is choked, and the diverging portion acts as a supersonic nozzle, determine the mass flow rate, in kg/s, and the Mach number, pressure, in bar, and temperature, in K, at the exit. Repeat if the diverging portion acts as a supersonic diffuser.

Answers

Alpha Geek
(8)
Status NEW Posted 15 May 2017 10:05 AM My Price 12.00

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Attachments

file 1494842788-Answer.docx preview (116 words )
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