Search

DIGITAL LIBRARY: SAMPE 2025 | INDIANAPOLIS, IN | MAY 19-22

Get This Paper

Experimental Characterization of Mode-II Interlaminar Fracture and Crack Arrestment in Geometrically Scaled Stitched Resin-Infused Composites under Thermal Loading

Description

Title: Experimental Characterization of Mode-II Interlaminar Fracture and Crack Arrestment in Geometrically Scaled Stitched Resin-Infused Composites under Thermal Loading

Authors: Yongjun So, Kwak Jin Bae, Han-Gyu Kim, Jaesang Yu

DOI: 10.33599/nasampe/s.25.0002

Abstract: This study investigates the enhanced mode-II interlaminar fracture toughness of stitched carbon fiber-reinforced plastics (CFRPs) for aerospace applications under high-temperature conditions and geometric size effects. For the experimental work, two different sizes of end-notched flexure (ENF) specimens were manufactured and tested using a three-point bending configuration. Additionally, three different temperature scenarios were designed using a heat gun and a heating chamber. The experimental data showed that the mechanical properties of the ENF specimens could be degraded under high-temperature environments. It was also shown that stitching is effective in preventing mechanical property degradation under different temperature regimes and geometric scales at different extents. Lastly, optical microscopic images revealed different types of delamination patterns in different geometric scales and the robustness of stitching yarns under mode-II interlaminar fracture conditions. Therefore, through-thickness stitching could contribute to enhancing the structural integrity of CFRP parts and structures subject to high-temperature conditions. For the aerospace applications of stitched composites under extreme environments, further study will be done to investigate the impact of different delamination patterns in geometrically-scaled stitched CFRPs on crack arrestment under high-temperature regimes.

References: 1. Gipson, L., “NASA Plans for Subsonic Flight Demonstrator,” https://www.nasa.gov/aeroresearch/nasa-plans-for-subsonic-flight-demonstrator, April 24, 2023. NASA, 2. Harrison, N. A., Hoffman, K., Lazzara, D. S., Reichenbach, E. Y., Sclafani, A. J., and Droney, C. K., “Subsonic Ultra Green Aircraft Research: Phase IV Final Report – Volume 1 Mach 0.80 Transonic Truss-Braced Wing High-Speed Design Report,” NASA/CR–20220016017, Vol. 1, October 2023. 3. Mason, B., Anderson, E., Cardona, A., Jutte C., and Larson, R., “Structural Sizing of a TowSteered Truss-Braced Wing Box Test Article”, AIAA-2025-0636, American Institute of Aeronautics and Astronautics (AIAA) Scitech, Orlando, FL, USA, January 6-10, 2025. 4. Cardona, A. M., Jegley, D. C., and Lovejoy, A. E., “Manufacturing Trials of Integrally Stiffened Composite Panels Using Automated Fiber Placement,” Society for the Advancement of Materials and Process Engineering (SAMPE) Conference and Exhibition, Seattle, WA, April 17-20, 2023, DOI: 10.33599/nasampe/s.23.0047. 5. Jegley, D., Lovejoy, A., Thrash, P., and Velicki, A., “History of Structural Stitching Development for Aerospace Applications,” AIAA 2024-2079, American Institute of Aeronautics and Astronautics (AIAA) Scitech, Orlando, FL, Jan 8-12, 2024, DOI: https://doi.org/10.2514/6.2024-2079. 6. Palmieri, F., Hudson, T., Cano, R., Tastepe, E., Rufeisen, D., Ahmed, L., Lin, Y., Wohl, C., Connell, J., “Reliable Bonding of Composite Laminates Using Reflowable Epoxy Resins,” Society for the Advancement of Materials and Process Engineering (SAMPE) Conference and Exhibition, Charlotte, NC, May 20-23, 2019, DOI: 10.33599/nasampe/s.19.1416. 7. Anonymous, PATRAN User Guide, MSC Software, Santa Ana, CA. 8. Anonymous, NASTRAN Analysis Quick Reference Manual, MSC Software, Santa Ana, CA. 9. Anonymous, Abaqus Analysis User’s Guide, Dassault Systemes, Waltham, MA. 10. NASA ISAAC Fact Sheet, FS-2016-12-273-LaRC, 2021. 11. Lovejoy, A., “Improved Method for Increased-Rate Stitched Composites Manufacturing,” AIAA 2023-0778, American Institute of Aeronautics and Astronautics (AIAA) Scitech, National Harbor, MD, Jan 23-27, 2023, DOI: https://doi.org/10.2514/6.2023-0778. 12. Shah A., Lovejoy A., Sullivan R., and Drake D., “Pull-off Behavior of Stitched Composite TJoints”, Composites Part B, 288 (2025), DOI: https://doi.org/10.1016/j.compositesb.2024.111911 13. Vericut Composites Software Package, CGTech, Irvine, CA.

Conference: SAMPE 2025

Publication Date: 2025/05/19

SKU: TP25-0000000002

Pages: 15

Price: $30.00

Get This Paper