Scaling for a Static Nonlinear Response of a Joined-Wing Aircraft

Scaling for a Static Nonlinear Response of a Joined-Wing Aircraft

Author(s):

V. Bond ( 716th Test and Evaluation Squadron, Arnold AFB, TN )
R. Canfield ( Air Force Institute of Technology, Wright Patterson Air Force Base, OH )
J. Cooper ( University of Liverpool, Liverpool, Great Britain )
M. Blair ( United States Air Force Research Laboratory, Wright Patterson Air Force Base, OH )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Multidisciplinary Analysis and Optimization Conference

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-5849

Paper no.:

AIAA 2008-5849

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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