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Shell Buckling Design Criteria Based on Manufacturing Imperfection SignaturesAn analysis-based approach .for developing shell-buckling design criteria for laminated-composite cylindrical shells that accurately accounts for the effects of initial geometric imperfections is presented. With this approach, measured initial geometric imperfection data from six graphite-epoxy shells are used to determine a manufacturing-process-specific imperfection signature for these shells. This imperfection signature is then used as input into nonlinear finite-element analyses. The imperfection signature represents a "first-approximation" mean imperfection shape that is suitable for developing preliminary-design data. Comparisons of test data and analytical results obtained by using several different imperfection shapes are presented for selected shells. Overall, the results indicate that the analysis-based approach presented for developing reliable preliminary-design criteria has the potential to provide improved, less conservative buckling-load estimates, and to reduce the weight and cost of developing buckling-resistant shell structures.
Document ID
20040077039
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Hilburger, Mark W.
(NASA Langley Research Center Hampton, VA, United States)
Nemeth, Michael P.
(NASA Langley Research Center Hampton, VA, United States)
Starnes, James H., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 2004
Subject Category
Structural Mechanics
Report/Patent Number
L-19007
NASA/TM-2004-212659
Report Number: L-19007
Report Number: NASA/TM-2004-212659
Meeting Information
Meeting: 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Norfolk, VA
Country: United States
Start Date: April 1, 2003
Sponsors: American Society of Mechanical Engineers, American Society for Composites, American Society of Civil Engineers, American Helicopter Society, Inc., American Inst. of Aeronautics and Astronautics
Funding Number(s)
WORK_UNIT: WU 23-719-20-30
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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