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Interlaminar R-Curve Effects in Thermoplastic Composites: Experiments and Model CorrelationsThe interlaminar fracture behavior of thermoplastic composites under Mode-I and Mode-II static loading is investigated in this research. The material system under consideration is a carbon fiber reinforced low melt semi-crystalline resin TC1225 LMPAEK T700G (T700/LMPAEK)†. Characterization experiments were conducted to measure the load-displacement response, peak load, and propagation of delamination from a pre-implanted Kapton® insert. The Mode-I response was characterized using a double cantilever beam (DCB) test according to the ASTM D5528-22 standard. It was observed that the propagation exhibited significant resistance to delamination growth, i.e., an R-Curve effect. The test data indicated that the steady-state fracture toughness, GSSI, was approximately twice the mean initiation fracture toughness, GIc. The Mode-II response of an end notch flexure (ENF) specimen tested according to the ASTM D7905-19 standard exhibited an unexpected stable behavior upon attaining peak load. Prior to attaining peak load, the Mode-II response exhibited some non-linearity, which may be attributed to nonlinear bulk material response, e.g., hyper-elasticity, viscoelasticity, plasticity, etc., and potentially friction at the load/support rollers and R-Curve effects.

Finite element models based on the Cohesive Zone Method (CZM) and the Virtual Crack Closure Technique (VCCT) were used to predict the DCB and ENF specimen responses. DCB analysis results obtained using GSSI predicted propagation consistent with experimental data. However, results obtained with the as characterized GIc were inaccurate in predicting delamination growth onset and peak load. ENF analysis results obtained with the as-characterized Mode-II fracture toughness, GIIc, were inaccurate in predicting the peak load and propagation. Hence, R-Curve effects were included in both DCB and ENF simulations, which enabled improved predictions. The experimentally determined Mode-I R-Curve was used for the DCB simulations, whereas an R-Curve was derived for Mode-II assuming that the change in compliance of the specimen was associated with crack growth only.
Document ID
20230008518
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Prabhakar M Rao
(Raytheon (United States) Waltham, Massachusetts, United States)
Carlos G Davila
(Langley Research Center Hampton, Virginia, United States)
Ronald Krueger
(National Institute of Aerospace Hampton, Virginia, United States)
William M Johnston
(Langley Research Center Hampton, Virginia, United States)
James G Ratcliffe
(Langley Research Center Hampton, Virginia, United States)
Cheryl A Rose
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
June 2, 2023
Subject Category
Composite Materials
Meeting Information
Meeting: American Society for Composites 38th Technical Conference
Location: Lowell, MA
Country: US
Start Date: September 17, 2023
End Date: September 20, 2023
Sponsors: American Society for Composites
Funding Number(s)
WBS: 816088.04.07.03
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
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