The supersonic nozzle of Fig P9.138 is over expanded (case G of Fig. 9.12) with Ae/At =

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The supersonic nozzle of Fig P9.138 is over expanded (case G of Fig. 9.12) with Ae/At = 3.0 and a stagnation pressure of 350 kPa. If the jet edge makes a 4° angle with the nozzle centerline, what is the back pressure pr in kPa?

The supersonic nozzle of Fig P9.138
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Fundamentals of Thermodynamics

ISBN: 978-0471152323

6th edition

Authors: Richard E. Sonntag, Claus Borgnakke, Gordon J. Van Wylen

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