Modeling of Structural Deflections on a F/A-18 Aircraft Following Flight Flutter Tests by Use of Subspace Identification Method

Modeling of Structural Deflections on a F/A-18 Aircraft Following Flight Flutter Tests by Use of Subspace Identification Method

Author(s):

S. De Jesus Mota ( Ecole de technologie superieure, Montreal, Quebec, Canada )
M. Nadeau-Beaulieu
R. Botez
M. Brenner ( NASA Dryden Flight Research Center, Edwards, CA )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Atmospheric Flight Mechanics Conference

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-6303

Paper no.:

AIAA Paper 2007-6303

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200719 [CD-ROM 2007 Disc 19]

Type:

Technical Paper

Details

TDL ID:	ZA00049511
Series ID:	PA00000162
Conf. info. (Name):	AIAA Atmospheric Flight Mechanics Conference and Exhibit
Conf. info. (Number):	2007
Conf. info. (Venue):	Hilton Head, South Carolina
Conf. info. (Date):	2007.08.20-2007.08.23
Note for article:	AIAA Atmospheric Flight Mechanics Conference and Exhibit, Hilton Head, South Carolina, Aug. 20-23, 2007

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