Open AccessImpact of inlet flow angle variation on the performance of a transonic compressor blade using NIPC
Author(s) -
Zeshuai Chen,
Zhiheng Xia,
Jiaqi Luo
Publication year - 2022
Publication title -
aip advances
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.421
H-Index - 58
ISSN - 2158-3226
DOI - 10.1063/5.0074200
Subject(s) - transonic , inlet , rotor (electric) , flow (mathematics) , mechanics , mass flow , gas compressor , polynomial chaos , turbomachinery , computer science , mathematics , monte carlo method , aerospace engineering , physics , engineering , mechanical engineering , aerodynamics , statistics
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