Setting the inlet conditions for a scramjet combustor
Question concerning inlet conditions.
I am given the following information for a scramjet combustor: stagnation temperature and stagnation pressure of the free stream, and the inlet Mach number.
Should a pressure-far-field or pressure inlet be used?
If a pressure-far-field inlet can someone help out in setting the gauge static pressure?
If a pressure inlet can someone help out in setting the supersonic/initial gauge pressure?
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