What is the back pressure pr in kpa


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Q: The supersonic nozzle is over expanded 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? You must solve the problem step by step and use APA format.

715_Supersonic nozzle.jpg

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Mechanical Engineering: What is the back pressure pr in kpa
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