Aerospike Nozzle, external flow
I am doing analysis over aerospike nozzle but getting trouble with Supersonic gauge pressure and operating pressure. As I am new to fluent, can anyone please tell what is Supersonic gauge pressure and what it should be. And how to set operating condition for 51000ft.
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It's the static pressure at that boundary. It's only needed if that boundary is supersonic.
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My Chamber pressure is 300psi so what should be my Supersonic gauge pressure for Supersonic boundry
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