Buckling of Laminated Composite Plates Subjected to Combined In-Plane Bi-Axial and Shear Loads

Buckling of Laminated Composite Plates Subjected to Combined In-Plane Bi-Axial and Shear Loads

Author(s):: Rastogi, Naveen ( Spirit AeroSystems, Inc., 3801 S. Oliver St., MC #K25-52, Wichita, KS 67210. )
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.:: 2009-2453
Paper no.:: AIAA Paper 2009-2453
Pages:: 18
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/10.2514/6.2009-2453

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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