Effect of oscillating leading-edge flaps on vortices over a delta wing

Effect of oscillating leading-edge flaps on vortices over a delta wing

Author(s):

Deng, Q. ( University of Cincinnati )
Gursul, I.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA Fluid Dynamics Conference

Ser. no.:

1997

Pub. Year:

1997

No.:

97-1972

Paper no.:

97-1972

Page(from):

1

Page(to):

9

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050846
Series ID:	PA00000147
Conf. info. (Name):	AIAA Fluid Dynamics Conference ; AIAA Shear Flow Control Conference
Conf. info. (Number):	28th ; 4th
Conf. info. (Venue):	Snowmass Village, CO
Conf. info. (Date):	1997.06.29-1997.07.02
Note for article:	28th AIAA Fluid Dynamics Conference, 4th AIAA Shear Flow Control Conference, June 29-July 2, 1997, Snowmass Village, CO

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