NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Buckling and Failure of Compression-loaded Composite Cylindrical Shells with Reinforced CutoutsResults from a numerical and experimental study that illustrate the effects of selected cutout reinforcement configurations on the buckling and failure response of compression-loaded composite cylindrical shells with a cutout are presented. The effects of reinforcement size, thickness, and orthotropy on the overall response of compression-loaded shells are described. In general, reinforcement around a cutout in a compression-loaded shell can retard or eliminate the local buckling response and material failure near the cutout and increase the buckling load of the shell. However, some results show that certain reinforcement configurations can cause a significant increase in the local interlaminar failures that can accumulate near the free edges of a cutout during a local buckling event.
Document ID
20050198887
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Hilburger, Mark W.
(NASA Langley Research Center Hampton, VA, United States)
Nemeth, Michael P.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Structural Mechanics
Report/Patent Number
AIAA Paper 2005-2370
Report Number: AIAA Paper 2005-2370
Meeting Information
Meeting: 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Austin, TX
Country: United States
Start Date: April 18, 2005
End Date: April 21, 2005
Sponsors: American Helicopter Society, Inc., American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, American Society of Civil Engineers, American Society for Composites
Funding Number(s)
OTHER: 23-376-70-30
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available