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
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