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Fig. 3 | Advances in Aerodynamics

Fig. 3

From: Recent investigations of shock wave effects and interactions

Fig. 3

a Instantaneous shadowgraph image showing shock wave characteristics. Rectangles mark the locations of the pixels in the downstream boundary layer and on the shock wave associated with magnitude squared coherence determination. b Magnitude squared coherence variation with frequency of data associated with locations near the shock wave and in the downstream boundary layer

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