Boundary layer development in axial compressors and turbines part 3 of 4: LP turbines

Boundary layer development in axial compressors and turbines part 3 of 4: LP turbines

Author(s):

Halstead, David E. ( GE Aircraft Engines )

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

1995

Pub. Year:

1995

No.:

95-GT-463

Paper no.:

95-GT-463

Pub. info.:

New York: The American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00002361
Series ID:	PA00000136
Note for article:	Presented at the International Gas Turbine and Aeroengine Congress and Exposition Houston, Texas - June 5-8, 1995 This paper hs been accepted for publication in the Transactions of the ASME Discussion of it will be accepted at ASME Headquarters until September 30, 1995

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