Robust Multi-fidelity Aerodynamic Design Optimization Using Surrogate Models

Robust Multi-fidelity Aerodynamic Design Optimization Using Surrogate Models

Author(s):

D. Jaeggi ( University of Cambridge, Cambridge, England, United Kingdom )
G. Parks
W. Dawes
J. Clarkson

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Multidisciplinary Analysis and Optimization Conference

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-6052

Paper no.:

AIAA 2008-6052

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200812 [CD-ROM 2008 Disc 12]

Type:

Technical Paper

Details

TDL ID:	ZA00050891
Series ID:	PA00000051
Conf. info. (Name):	AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
Conf. info. (Number):	12th
Conf. info. (Venue):	Victoria, Britith Columbia, Canada
Conf. info. (Date):	2008.09.10-2008.09.12

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