Index of Measures

boundary layer total pressure rake
 
 
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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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Similar Measures

Subsequent references to data sheets are given which describe with high probability similar measured values. The selection is made on the basis of semantic affinity: