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Question
In a closed-circuit supersonic wind tunnel, the convergent-divergent (C-D) nozzle and test section are followed by a C-D diffuser to swallow the starting shock. Here, we should have the
Options:
A .  diffuser throat larger than the nozzle throat and the shock located just at the diffuser throat.
B .  diffuser throat larger than the nozzle throat and the shock located downstream of the diffuser throat.
C .  diffuser throat of the same size as the nozzle throat and the shock located just at the diffuser throat.
D .  diffuser throat of the same size as the nozzle throat and the shock located downstream of the diffuser throat.
Answer: Option B


-NA-



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