Wake vorticity decay and blade response in an axial compressor with varying axial gap

Wake vorticity decay and blade response in an axial compressor with varying axial gap

Author(s):

Wo, A.M. ( National Taiwan University )
Chung, M.H.
Chang, S.J.
Lee, S.F.

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

1999

Pub. Year:

1999

No.:

99-GT-451

Paper no.:

99-GT-451

Pub. info.:

New York: The American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00002782
Series ID:	PA00000136
Conf. info. (Name):	International Gas Turbine & Aeroengine Congress & Exhibition
Conf. info. (Number):	1999
Conf. info. (Venue):	Indianapolis, Indiana
Conf. info. (Date):	1999.06.07-1999.06.10
Note for article:	Presented at the International Gas Turbine & Aeroengine Congress & Exhibition Indianapolis, Indiana - June 7-June 10, 1999

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