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Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, v.229 no.12, 2015년, pp.2221 - 2230
Feng, Yanyan , Song, Yanping , Chen, Fu , Liu, Huaping
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As a 50° camber angle compressor cascade being the object, the numerical investigations of the endwall vortex generator jets effect on flow separation control were conducted. The results show that the flow separation is significantly weakened and the maximum total pressure loss reduction is 9...
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ASME J Nerger D 1 134 021010 2012
Chen SW. Experimental and numerical investigation of using bowed blade in compressor cascade with different turning angles . PhD Thesis, Harbin Institute of Technology, China, 2007.
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