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?
Asked
Active
Viewed 67 times
0
-
2You should ask "please" at least seven time to get an answer – sophit Oct 31 '23 at 20:31
-
1Isn't this the same as your last question https://aviation.stackexchange.com/q/101538/7532 – Ralph J Oct 31 '23 at 21:08