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Experimental Investigation of the Three-Dimensional Structure of a Shock Wave/Turbulent Boundary Layer Interaction

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Figure

Table 1. Summary of experimental conditions.
Figure 3. Instantaneous velocity distributions at z/δ=0.12: (a) u/U ∞ ; (b)  v/U ∞ ; (c) w/U ∞
Figure 4. Instantaneous flow organization of the interaction. Isosurfaces  of streamwise velocity are shown; relatively high-speed (0.9U ∞ ) in red,  intermediate (0.75U ∞ ) in green, and relatively low-speed (0.55U ∞ ) in  blue
Figure 5. Modal energy content for the kth eigenmode and cumulative  modal energy content for the Kth cumulative sum
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