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Effects of the Inlet Boundary Layer Thickness on the Rotating Stall in an Axial Compressor

Title
Effects of the Inlet Boundary Layer Thickness on the Rotating Stall in an Axial Compressor
Authors
백제현
Date Issued
9-Jun-2008
Publisher
ASME
URI
http://oasis.postech.ac.kr/handle/2014.oak/58314
Article Type
Conference
Citation
ASME Turbo Expo 2008, 2008-06-09
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