Investigation Into Scale Effects on the Performance of Sub Boundary-Layer Vortex Generators on Civil Aircraft High-Lift Devices.

Investigation Into Scale Effects on the Performance of Sub Boundary-Layer Vortex Generators on Civil Aircraft High-Lift Devices.

Author(s):

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA Fluid Dynamics Conference

Ser. no.:

2002

Pub. Year:

2002

No.:

2002-3274

Paper no.:

2002-3274

Pages:

6

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00001702
Series ID:	PA00000147
Conf. info. (Name):	AIAA Fluid Dynamics Conference and Exhibit
Conf. info. (Number):	32nd
Conf. info. (Venue):	St. Louis, MO
Conf. info. (Date):	2002.06.24-2002.06.26
Note for article:	32nd AIAA Fluid Dynamics Conference and Exhibit, St. Louis, Missouri, 24-26 June 2002

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