TY - JOUR
T1 - Leakage performance of CFRP laminate under cryogenic temperature
T2 - Experimental and simulation study
AU - Meng, Jinxin
AU - Zheng, Huayong
AU - Wei, Yong
AU - Liu, Debo
AU - Shi, Hanqiao
AU - Wang, Panding
AU - Lei, Hongshuai
AU - Fang, Daining
N1 - Publisher Copyright:
© 2022 Elsevier Ltd
PY - 2022/7/28
Y1 - 2022/7/28
N2 - Leakage rate prediction of carbon fiber reinforced polymer (CFRP) composites for cryogenic propellant tanks has been a challenge for the research community. In this paper, the leakage properties of CFRP laminates with various lay-up configurations are experimentally assessed by measuring their leakage rates under different loads and temperatures. The effects of temperature, cooling conditions and loading on the leakage rates of the above laminate composites are discussed. Meanwhile, in-situ micro X-ray computed tomography (μCT) testing is performed to characterize the internal microstructure evolution of the composites under tension. The geometric morphology and parameters of defects are investigated as well. The propagation of internal cracks in the composites under loading is carefully monitored. A novel 3D image-based model is developed using μCT scans to predict the leakage properties of the composites under various loads. The initiation and propagation leakage rates of laminates, whose values are found to be within the same order of magnitude as experimental ones. The proposed simulation method allows one to quickly calculate the image-based leakage model suitable for the prediction of leakage performance and the lay-up design of composite cryogenic propellant tanks under cryogenic temperatures.
AB - Leakage rate prediction of carbon fiber reinforced polymer (CFRP) composites for cryogenic propellant tanks has been a challenge for the research community. In this paper, the leakage properties of CFRP laminates with various lay-up configurations are experimentally assessed by measuring their leakage rates under different loads and temperatures. The effects of temperature, cooling conditions and loading on the leakage rates of the above laminate composites are discussed. Meanwhile, in-situ micro X-ray computed tomography (μCT) testing is performed to characterize the internal microstructure evolution of the composites under tension. The geometric morphology and parameters of defects are investigated as well. The propagation of internal cracks in the composites under loading is carefully monitored. A novel 3D image-based model is developed using μCT scans to predict the leakage properties of the composites under various loads. The initiation and propagation leakage rates of laminates, whose values are found to be within the same order of magnitude as experimental ones. The proposed simulation method allows one to quickly calculate the image-based leakage model suitable for the prediction of leakage performance and the lay-up design of composite cryogenic propellant tanks under cryogenic temperatures.
KW - Composites laminates
KW - Cryogenic temperature
KW - Image-based simulation
KW - In-situ micro X-ray CT
KW - Leakage rate
UR - http://www.scopus.com/inward/record.url?scp=85130792209&partnerID=8YFLogxK
U2 - 10.1016/j.compscitech.2022.109550
DO - 10.1016/j.compscitech.2022.109550
M3 - Article
AN - SCOPUS:85130792209
SN - 0266-3538
VL - 226
JO - Composites Science and Technology
JF - Composites Science and Technology
M1 - 109550
ER -