Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering
2019 / 06
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The effect of endwall boundary layer and incoming wakes on secondary flow in a high-lift low-pressure turbine cascade at low Reynolds number
Qu, Xiao, Zhang, Yanfeng, Lu, Xingen, Lei, Zhijun, Zhu, JunqiangJournal:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
DOI:
10.1177/0954410019853994
Date:
June, 2019
File:
PDF, 2.66 MB
2019