Investigation of the Mechanical Behaviors and Damage Mechanism of C/C Composites Impacted by High-Velocity Jets

• Published in: Materials Vol. 17; no. 4; p. 963
• Main Authors: Yue, Yifan, Wang, Bo, Yan, Kefei, Zhao, Renxi, Zhang, Chengyu, Li, Yulong
• Format: Journal Article
• Language: English
• Published: Switzerland MDPI AG 01.02.2024
• Subjects: Ablation; Aircraft; C/C composites; Carbon; Composite materials; Computed tomography; damage mechanism; Delamination; Diameters; Experiments; High temperature; Hypersonic aircraft; Impact damage; Impact tests; Investigations; Jet aircraft; Jet impingement; Laminated materials; Leading edges; Mechanical properties; Nose cones; Optical microscopy; Rain erosion; Rain impact damage; Residual strength; Scanning electron microscopy; Spaceplanes; Three dimensional composites; Velocity; Wings (aircraft); United States > US; damage mechanism; residual strength; rain erosion; C/C composites
• ISSN: 1996-1944; 1996-1944
• DOI: 10.3390/ma17040963

Carbon/Carbon (C/C) composites exhibit excellent mechanical properties at high temperatures, making them widely used in aerospace, such as the leading edges of spaceplane wings and the nose cones of hypersonic aircraft. However, damage caused by rain erosion to C/C composites affects their mechanical properties and poses significant challenges during operational service periods. A jet impingement test platform was employed to conduct single and multiple water-jet erosion tests on three-dimensional orthogonal C/C composite materials and to investigate the residual mechanical properties of the specimens after jet impact. The damage was characterized using optical microscopy, scanning electron microscopy, and X-ray computed tomography. The results showed that the damage types of the C/C composite materials under water-jet impingement included fiber bundle fracturing, delamination, and debonding. The extent of erosion damage was positively correlated with the jet velocity and diameter. The changes in the multi-jet damage indicated a cumulative expansion process, and -directional fiber bundles exhibited superior resistance to jet impact damage propagation. The results of the three-point bending tests showed that the greater the initial impact damage, the lower the residual mechanical properties of the materials, and the residual strength of the specimen suddenly decreased when damage occurred at the back of the specimen.