Numerical Study of Aerodynamic Performance of Airfoils at Low Angles of Attack by Active Flow Control of Trailing Edge Vortices

Numerical Study of Aerodynamic Performance of Airfoils at Low Angles of Attack by Active Flow Control of Trailing Edge Vortices

Author(s):

J. Vadillo ( Washington University in St. Louis, St. Louis, MO )
R. Agarwal

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2006

Pub. Year:

2006

No.:

2006-1058

Paper no.:

AIAA Paper 2006-1058

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200604 [CD-ROM 2006 Disc 4]

Type:

Technical Paper

Details

TDL ID:	ZA00047219
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	44th
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2006.01.09-2009.01.12

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