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Impact Damage and Strain Rate Effects for Toughened Epoxy Composite StructuresStructural integrity of composite systems under dynamic impact loading is investigated herein. The GENOA virtual testing software environment is used to implement the effects of dynamic loading on fracture progression and damage tolerance. Combinations of graphite and glass fibers with a toughened epoxy matrix are investigated. The effect of a ceramic coating for the absorption of impact energy is also included. Impact and post impact simulations include verification and prediction of (1) Load and Impact Energy, (2) Impact Damage Size, (3) Maximum Impact Peak Load, (4) Residual Strength, (5) Maximum Displacement, (6) Contribution of Failure Modes to Failure Mechanisms, (7) Prediction of Impact Load Versus Time, and (8) Damage, and Fracture Pattern. A computer model is utilized for the assessment of structural response, progressive fracture, and defect/damage tolerance characteristics. Results show the damage progression sequence and the changes in the structural response characteristics due to dynamic impact. The fundamental premise of computational simulation is that the complete evaluation of composite fracture requires an assessment of ply and subply level damage/fracture processes as the structure is subjected to loads. Simulation results for the graphite/epoxy composite were compared with the impact and tension failure test data, correlation and verification was obtained that included: (1) impact energy, (2) damage size, (3) maximum impact peak load, (4) residual strength, (5) maximum displacement, and (6) failure mechanisms of the composite structure.
Document ID
20060021978
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Chamis, Christos C.
(NASA Glenn Research Center Cleveland, OH, United States)
Minnetyan, Levon
(Clarkson Univ. Potsdam, NY, United States)
Date Acquired
August 23, 2013
Publication Date
May 1, 2006
Subject Category
Composite Materials
Report/Patent Number
NASA/TM-2006-214253
E-15498
Report Number: NASA/TM-2006-214253
Report Number: E-15498
Funding Number(s)
WBS: WBS 754-02-07-03
Distribution Limits
Public
Copyright
Public Use Permitted.
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