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Experimental Investigation of the Effect of the Probe Support Tail Structure on the Compressor Cascade Flow Field
Experimental Investigation of the Effect of the Probe Support Tail Structure on the Compressor Cascade Flow Field
2019
Honghui Xiang
Ning Ge
Jie Gao
Rongfei Yang
Minjie Hou
Keywords:
Flow (psychology)
Engineering
Aerospace engineering
Tail structure
Cascade
Gas compressor
compressor cascade
flow field
Correction
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