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High-speed camera-based measurement system for aeroacoustic investigations

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Figure

Figure 1. Sketch of a perforated bias flow liner with a cavity be-hind, installed in a flow duct.
Figure 2. FM-DGV measurement principle: (a) and (b) the particles are illuminated from the direction i, and the scattered light is detectedbehind a caesium absorption cell
Table 1. Specifications of the measurement system including thelaser and the high-speed camera.
Figure 5. Measurement setup:using the FM-DGV system in combination with a high-speed camera
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