Index of Measures

visualisation of the boundary layer behaviour by means of Liquide Crystals
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Transonic Cascade Wind Tunnel (TGK)

Institute of Propulsion Technology

Experimental investigation of sub- and transonic flow through plane compressor cascade. The main task of the test facility is the exact determination of losses, performance parameters and working range of compressor profiles. Due to the very good optical and measuring accessibility, secondary flow phenomena can be studied in detail.

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