Index of Measures

angle and velocity (by means of L2F system)
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Transonic Cascade Wind Tunnel (TGK)

DLR 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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