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What is the back pressure pr

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The supersonic nozzle of Fig is over expanded (case G of Fig) 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?

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Reference no: EM13879239

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What is the back pressure pr : The supersonic nozzle of Fig is over expanded (case G of Fig) 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?
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