Abstract
Tests were carried out to determine the interlaminar fracture toughness of stitch-bonded biaxial polymer matrix carbon nanotube nanocomposites for mode I, II, and I-II including durability effects. Analysis of the test specimens in terms of mode I energy release rates showed good agreement among Modified Beam Theory, Compliance Calibration, and Modified Compliance Calibration methods. End-Notched Flexure (ENF) and four point End-Notched Flexure (4ENF) tests gave very consistent crack initiation and propagation results for mode II fracture. The results show that the critical mode I energy release rate for delamination decreases monotonically with increasing mode II loading. The effects of accelerated aging (60°C and 90% Rh) on fracture properties were studied. Early accelerated aging (0-12 months) has the dominant diminishing effect on energy release rate initiation and propagation in composites and nanocomposites.
Original language | English (US) |
---|---|
Title of host publication | Advances in Aerospace Technology |
Publisher | American Society of Mechanical Engineers (ASME) |
Volume | 1 |
ISBN (Electronic) | 9780791850510 |
DOIs | |
State | Published - 2016 |
Event | ASME 2016 International Mechanical Engineering Congress and Exposition, IMECE 2016 - Phoenix, United States Duration: Nov 11 2016 → Nov 17 2016 |
Other
Other | ASME 2016 International Mechanical Engineering Congress and Exposition, IMECE 2016 |
---|---|
Country/Territory | United States |
City | Phoenix |
Period | 11/11/16 → 11/17/16 |
ASJC Scopus subject areas
- Mechanical Engineering