Effect of Edge-Based Discretization Schemes in Computations of the DLR F6 Wing-Body Configuration

Effect of Edge-Based Discretization Schemes in Computations of the DLR F6 Wing-Body Configuration

Author(s):

P. Eliasson ( FOI, Swedish Defence Research Agency, Stockholm, Sweden )
J. Nordström
S. Peng

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Fluid Dynamics Conference

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-4153

Paper no.:

AIAA Paper 2008-4153

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200807 [CD-ROM 2008 Disc 7]

Type:

Technical Paper

Details

TDL ID:	ZA00050884
Series ID:	PA00000147
Conf. info. (Name):	AIAA Fluid Dynamics Conference and Exhibit
Conf. info. (Number):	38th
Conf. info. (Venue):	Seattle, WA
Conf. info. (Date):	2008.06.23-2008.06.26
Note for article:	38th Fluid Dynamics Conference and Exhibit, 23-26 June 2008, Seattle, Washington

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