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zoki85
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Typical supersonic airplane in supersonic flight creates 2 shock waves (2 Mach cones):
"N-shaped" shock wave.
How much of the "sound" energy near the shock waves region is contributed by the sound emmited from jet engines work?
"N-shaped" shock wave.
How much of the "sound" energy near the shock waves region is contributed by the sound emmited from jet engines work?