Predictions of Separated and Transitional Boundary Layers Under Low-Pressure Turbine Airfoil Conditions Using an Intermittency Transport Equation

Predictions of Separated and Transitional Boundary Layers Under Low-Pressure Turbine Airfoil Conditions Using an Intermittency Transport Equation

Author(s):

Suzen,Y.Bora ( University of Kentucky Department of Mechanical Engineering )
Huang,P.G. ( National Aeronautics and Space Administration Glenn Research Center )
Hultgren,Lennart S.
Ashpis,David E.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2001

Pub. Year:

2001

No.:

2001-0446

Paper no.:

AIAA-2001-0446

Page(from):

1

Page(to):

21

Pages:

21

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050880
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting & Exhibit
Conf. info. (Number):	39th
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2001.01.08-2001.01.11
Note for article:	39th AIAA Aerospace Sciences Meeting & Exhibit 8-11 January 2001/Reno, NV

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