Development of Boundary Layer on the Blade in an Axial Flow Compressor

Title
Development of Boundary Layer on the Blade in an Axial Flow Compressor
Authors
신유환김광호
Keywords
Boundary Layer; Multi-Stage Axial Compressor; Corner Separation; 경계층; 다단 축류 압축기; 모서리 박리
Issue Date
2004-08
Publisher
The 3rd National Congress on Fluids Engineering
URI
http://pubs.kist.re.kr/handle/201004/26009
Appears in Collections:
KIST Publication > Conference Paper
Files in This Item:
There are no files associated with this item.
Export
RIS (EndNote)
XLS (Excel)
XML


qrcode

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.

BROWSE