Adaptive mesh refinement method based investigation of the interaction between shock wave, boundary layer, and tip vortex in a transonic compressor
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Title
Adaptive mesh refinement method based investigation of the interaction between shock wave, boundary layer, and tip vortex in a transonic compressor
Authors
Keywords
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Journal
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING
Volume 232, Issue 4, Pages 694-715
Publisher
SAGE Publications
Online
2017-01-10
DOI
10.1177/0954410016687142
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