Multi-Fidelity Design Optimization Studies for Supersonic Jets Using Surrogate Management Frame Method

Multi-Fidelity Design Optimization Studies for Supersonic Jets Using Surrogate Management Frame Method

Author(s):

Choi, S. ( Stanford University, Stanford, CA )
Alonso, J.
Kroo, I.

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Applied Aerodynamics Conference

Ser. no.:

23rd

Pub. Year:

2005

No.:

2005-5077

Paper no.:

AIAA Paper 2005-5077

Pub. info.:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200511 [CD-ROM 2005 Disc 11]

Type:

Technical Paper

Details

TDL ID:	ZA00001627
Series ID:	PA00000157
Conf. info. (Name):	AIAA Applied Aerodynamics Conference
Conf. info. (Number):	23rd
Conf. info. (Venue):	Toronto, Ontario
Conf. info. (Date):	2005.06.06

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