I can’t find a simple explanation of how the pressure waves propagate that leads to a shock over an aerofoil online.
How does this happen with upstream flow that is high speed but subsonic?
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2$\begingroup$ You should ask "please" at least seven time to get an answer 😉 $\endgroup$– sophitOct 31 at 20:31
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1$\begingroup$ Isn't this the same as your last question aviation.stackexchange.com/q/101538/7532 $\endgroup$– Ralph J ♦Oct 31 at 21:08
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