High-Lift Wing Design in Consideration of Sweep Angle Effect Using Kriging Model

Author(s):

• M. Kanazaki ( Japan Aerospace Exploration Agency, Mitaka, Tokyo, Japan )
• T. Imamura
• S. Jeong ( Tohoku University, Sendai, Japan )
• K. Yamamoto ( Japan )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-0175

Paper no.:

AIAA Paper 2008-0175

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