Effects of the Inlet Boundary Layer Thickness on the Flow and Loss Characteristics in an Axial Compressor.

Effects of the Inlet Boundary Layer Thickness on the Flow and Loss Characteristics in an Axial Compressor.

Author(s):

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

2005

Pub. Year:

2005

No.:

GT2005-68580

Paper no.:

GT2005-68580

Pages:

11

Pub. info.:

New York, NY: American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00001650
Series ID:	PA00000136
Conf. info. (Name):	ASME Turbo Expo 2005
Conf. info. (Number):	2005
Conf. info. (Venue):	Reno-Tahoe, NV., USA
Conf. info. (Date):	2005.06.06-2005.06.09
Note for article:	ASME Turbo Expo 2005, Reno-Tahoe, NV., USA, June 6-9, 2005

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