@inproceedings{fbec6546f1a3436e8b4650c97adf44cb,
title = "Numerical investigation of secondary flows through highly loaded transonic turbine stage",
abstract = "The turbine aero-thermal design expertise has not reached the ultimate level in comparison to compressor expertise which has evolved to high loading, high pressure ratio design with a limited number of stages. For high pressure turbine section, single highly loaded stages are typically representative of wide class of advanced aero engines. The transonic turbines significantly operate at higher pressure ratios with less number of stages but at an expense of relatively lower efficiencies.",
keywords = "highly loaded, numerical investigation, secondary flow, tip leakage, transonic turbine",
author = "Asghar, \{Muhammad Afzaal\} and Lu Lipeng and Yangwei Liu and Su Zhi",
note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 14th International Bhurban Conference on Applied Sciences and Technology, IBCAST 2017 ; Conference date: 10-01-2017 Through 14-01-2017",
year = "2017",
month = mar,
day = "1",
doi = "10.1109/IBCAST.2017.7868104",
language = "英语",
series = "Proceedings of 2017 14th International Bhurban Conference on Applied Sciences and Technology, IBCAST 2017",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "530--538",
editor = "Muhammad Zafar-uz-Zaman",
booktitle = "Proceedings of 2017 14th International Bhurban Conference on Applied Sciences and Technology, IBCAST 2017",
address = "美国",
}