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Probabilistic Simulation of Progressive Fracture in Bolted-Joint Composite LaminatesThis report describes computational methods to probabilistically simulate fracture in bolted composite structures. An innovative approach that is independent of stress intensity factors and fracture toughness was used to simulate progressive fracture. The effect of design variable uncertainties on structural damage was also quantified. A fast probability integrator assessed the scatter in the composite structure response before and after damage. Then the sensitivity of the response to design variables was computed. General-purpose methods, which are applicable to bolted joints in all types of structures and in all fracture processes-from damage initiation to unstable propagation and global structure collapse-were used. These methods were demonstrated for a bolted joint of a polymer matrix composite panel under edge loads. The effects of the fabrication process were included in the simulation of damage in the bolted panel. Results showed that the most effective way to reduce end displacement at fracture is to control both the load and the ply thickness. The cumulative probability for longitudinal stress in all plies was most sensitive to the load; in the 0 deg. plies it was very sensitive to ply thickness. The cumulative probability for transverse stress was most sensitive to the matrix coefficient of thermal expansion. In addition, fiber volume ratio and fiber transverse modulus both contributed significantly to the cumulative probability for the transverse stresses in all the plies.
Document ID
19960027037
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Minnetyan, L.
(Clarkson Univ. Potsdam, NY United States)
Singhal, S. N.
(NYMA, Inc. Brook Park, OH United States)
Chamis, C. C.
(NASA Lewis Research Center Cleveland,OH United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1996
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:107107
NASA-TM-107107
E-10004
Report Number: NAS 1.15:107107
Report Number: NASA-TM-107107
Report Number: E-10004
Meeting Information
Meeting: Structures, Structural Dynamics and Materials Conference
Location: Hilton Head, SC
Country: United States
Start Date: April 18, 1994
End Date: April 20, 1994
Sponsors: American Society of Civil Engineers, American Society of Mechanical Engineers, American Helicopter Society, Inc., American Inst. of Aeronautics and Astronautics
Accession Number
96N28536
Funding Number(s)
PROJECT: RTOP 505-63-5B
CONTRACT_GRANT: NAS3-27186
Distribution Limits
Public
Copyright
Public Use Permitted.
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