Utilization of Response Surface Methodologies in the Multi-Discipline Design Optimization of an Aircraft Wing.

Utilization of Response Surface Methodologies in the Multi-Discipline Design Optimization of an Aircraft Wing.

Author(s):

Publication title:

2009 SAE world congress : technical paper

Title of ser.:

Society of Automotive Engineers technical paper series

Ser. no.:

2009

Pub. Year:

2009

No.:

2009-01-0344

Paper no.:

2009-01-0344

Pages:

9

Pub. info.:

Warrendale, Penn.: Society of Automotive Engineers

ISSN:

01487191

Language:

English

Call no.:

S10400

Type:

Technical Paper

Details

TDL ID:	ZA00052095
Series ID:	PA00000058
Conf. info. (Name):	SAE World Congress & Exhibition, 2009
Conf. info. (Number):	2009
Conf. info. (Venue):	Detroit, MI, USA
Conf. info. (Date):	2009.04.20-2009.04.23
Note for article:	SAE 2009 World Congress, April 20-23, 2009, Detroit, Michigan, USA

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