Pre-Buckling and Buckling of Unsymmetrically- Laminated Stiffened Composite Panels with Stringer Terminations Under In-Plane Loads

Pre-Buckling and Buckling of Unsymmetrically- Laminated Stiffened Composite Panels with Stringer Terminations Under In-Plane Loads

Author(s):

Cosentino, Enzo ( Airbus UK Ltd. Golf Course Lane, Bristol BS34 7AR, England, United Kingdom )
Weaver, Paul ( University of Bristol, Queen’s Building, University Walk, Bristol BS8 1TR l, England, United Kingdom )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Ser. no.:

2009

Pub. Year:

2009

No.:

2009-2455

Paper no.:

AIAA Paper 2009-2455

Pages:

31

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200905

Type:

Technical Paper

Link(DOI, etc.)

http://doi.org/10.2514/6.2009-2455

Details

TDL ID:	ZA00066595
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Conf. info. (Number):	50th
Conf. info. (Venue):	Palm Springs, California
Conf. info. (Date):	2009.05.04-2009.05.07
Note for article:	50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 17th 4-7 May 2009, Palm Springs, California

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