Numerical Simulation of Half-Span Aircraft Model with High-Lift Devices in Wind Tunnel

Numerical Simulation of Half-Span Aircraft Model with High-Lift Devices in Wind Tunnel

Author(s):

M. Murayama ( Japan Aerospace Exploration Agency, Tokyo, Japan )
Y. Yokokawa
K. Tanaka ( Ryoyu Systems Company, Ltd., Tokyo, Japan )
K. Yamamoto ( Japan Aerospace Exploration Agency, Tokyo, Japan )
T. Ito

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-0333

Paper no.:

AIAA Paper 2008-0333

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200801 [CD-ROM 2008 Disc 1]

Type:

Technical Paper

Details

TDL ID:	ZA00049519
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	46th
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2008.01.07-2008.01.10
Note for article:	46th AIAA Aerospace Sciences Meeting and Exhibit, 7-10 January 2008, Reno, Nevada

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