Experimental Investigation of the Effect of the Probe Support Tail Structure on the Compressor Cascade Flow Field
Xiang, Honghui, Ge, Ning, Gao, Jie, Yang, Rongfei, Hou, MinjieLanguage:
english
Journal:
International Journal of Turbo & Jet-Engines
DOI:
10.1515/tjj-2016-0071
Date:
January, 2016
File:
PDF, 3.11 MB
english, 2016