Engineering, 22.10.2019 23:50 mari8493
You are designing a supersonic inlet that uses one oblique shock followed by a normal shock and you are comparing two designs. one uses an oblique shock that turns the flow 10 degrees followed by a normal shock while the other uses an oblique shock that turns the flow 25 degrees followed by a normal shock. for a flight mach number of 2.5, which design gives the smaller drop in stagnation pressure through the two shocks?
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You are designing a supersonic inlet that uses one oblique shock followed by a normal shock and you...
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