Role of blade passage flow structures in axial compressor rotating stall inception

Role of blade passage flow structures in axial compressor rotating stall inception

Author(s):

Hoying, Donald A. ( Air Force Research Laboratory )
Tan, Choon S.
Vo, Huu Duc
Greitzer, Edward M.

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

1998

Pub. Year:

1998

No.:

98-GT-588

Paper no.:

98-GT-588

Pub. info.:

New York: The American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00002886
Series ID:	PA00000136
Conf. info. (Name):	International Gas Turbine & Aeroengine Congress & Exhibition
Conf. info. (Number):	1998
Conf. info. (Venue):	Stockholm, Sweden
Conf. info. (Date):	1998.06.02-1998.06.05
Note for article:	Presented at the International Gas Turbine & Aeroengine Congress & Exhibition Stockholm, Sweden - June 2-June 5, 1998

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