Exam (elaborations)
Propulsion|2023 LATEST UPDATE|GUARANTEED SUCCESS
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Stagnation Temperature _____ across a shock remains constant What is Rayleigh flow? Flow that is 1-D, quasi-equilibrium, with heat removal or addition. Usually in a combustor. What does the regression rate depend on? Chamber Pressure, r_dot = alpha *P^n Stagnation Pressure _...
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