Citation: | ZHANG Hongyu, QIAN Zhen, NIU Bo, et al. Mechanical properties and fracture mechanisms of low-density fiber preforms reinforced phenolic aerogel composites[J]. Acta Materiae Compositae Sinica, 2022, 39(8): 3663-3673. doi: 10.13801/j.cnki.fhclxb.20210909.002 |
[1] |
喻成璋, 刘卫华. 高超声速飞行器气动热预测技术研究进展[J]. 航空科学技术, 2021, 32(2): 14-21.
YU Chengzhang, LIU Weihua. Research status of aeroheating prediction technology for hypersonic aircraft[J]. Aeronautical Science and Technology, 2021, 32(2): 14-21(in Chinese).
|
[2] |
ALLEN H J. Hypersonic flight and the reentry problem: The twenty-first wright brothers lecture[J]. Journal of the Aerospace Sciences,1958,25(4):217-227. doi: 10.2514/8.7600
|
[3] |
KARIMI M S, OBOODI M J. Investigation and recent deve-lopments in aero dynamic heating and drag reduction for hypersonic flows[J]. Heat and Mass Transfer, 2019, 55(2): 547-569.
|
[4] |
韩杰才, 洪长青, 张幸红, 等. 新型轻质热防护复合材料的研究进展[J]. 载人航天, 2015, 21(4): 315-321
HAN Jiecai, HONG Changqing, ZHANG Xinghong, et al. Research progress of novel lightweight thermal protection composites[J]. Manned Spaceflight, 2015, 21(4): 315-321(in Chinese).
|
[5] |
薛华飞, 姚秀荣, 程海明, 等. 热防护用轻质烧蚀材料现状与发展[J]. 哈尔滨理工大学学报, 2017, 22(1):123-128.
XUE Huafei, YAO Xiurong, CHENG Haiming, et al. Current status and development of light ablative materials for thermal protection[J]. Journal of Harbin University of Science and Technology,2017,22(1):123-128(in Chinese).
|
[6] |
LACHAUD J, COZMUTA I, MANSOUR N N. Multiscale approach to ablation modeling of phenolic impregnated carbon ablators[J]. Journal of Spacecraft and Rockets,2010,47(6):910-921. doi: 10.2514/1.42681
|
[7] |
NATALI M, PURI I, KENNY J M, et al. Microstructure and ablation behavior of an affordable and reliable nanostructured phenolic impregnated carbon ablator (PICA)[J]. Polymer Degradation and Stability, 2017, 141: 84-96.
|
[8] |
TRAN H K, RASKY D J, ESFAHANI L. Thermal response and ablation characteristics of lightweight ceramic ablators[J]. Journal of Spacecraft and Rockets,1994,31(6):993-998. doi: 10.2514/3.26549
|
[9] |
RIVIER M, LACHAUD J, CONGEDO P M. Ablative thermal protection system under uncertainties including pyrolysis gas composition[J]. Aerospace Science and Technology, 2019, 84: 1059-1069.
|
[10] |
MEURISSE J B E, LACHAUD J, PANERAI F, et al. Multidimensional material response simulations of a full-scale tiled ablative heat shield[J]. Aerospace Science and Technology, 2018, 76: 497-511.
|
[11] |
LIU X, SUN J, YUAN F, et al. Lightweight, flexible, and heat-insulated phenolic impregnated carbon ablator (PICA) with adjustable flexibility and high compressive resilience property[J]. Journal of Applied Polymer Science, 2022, 139(9): 51712.
|
[12] |
ZHNG J, FANG G D, YANG L W, et al. Comparison of abla-tive and compressive mechanical behavior of several PICA-like ablative materials[J]. Science China Technological Sciences, 2020, 63(8): 1478-1486.
|
[13] |
程海明. 新型超轻质碳/酚醛烧蚀复合材料的制备与性能研究[D]. 哈尔滨: 哈尔滨工业大学, 2017.
CHENG Haiming. Preparation and properties of novel ultra-lightweight carbon/phenolic ablation composites[D]. Harbin: Harbin Institute of Technology, 2017(in Chinese).
|
[14] |
WHITE S M. High-temperature spectrometer for thermal protection system radiation measurements[J]. Journal of Spacecraft and Rockets, 2010, 47(1): 21-28.
|
[15] |
刘建军, 李铁虎, 郝志彪, 等. 针刺炭布/网胎复合织物的组分形态及性能研究[J]. 固体火箭技术, 2005, 28(4):299-302. doi: 10.3969/j.issn.1006-2793.2005.04.016
LIU Jianjun, LI Tiehu, HAO Zhibiao, et al. Study on composition morphology and properties of acupuncture carbon fabric/mesh pad composite fabric[J]. Solid Rocket Technology,2005, 28(4):299-302(in Chinese). doi: 10.3969/j.issn.1006-2793.2005.04.016
|
[16] |
朱召贤, 董金鑫, 贾献峰, 等. 酚醛气凝胶/炭纤维复合材料的结构与烧蚀性能[J]. 新型炭材料, 2018, 33(4):370-376.
ZHU Zhaoxian, DONG Jinxin, JIA Xianfeng, et al. Structure and ablation properties of phenolic aerogel/carbon fiber composites[J]. New Carbon Materials,2018,33(4):370-376(in Chinese).
|
[17] |
董金鑫, 朱召贤, 姚鸿俊, 等. 酚醛气凝胶/碳纤维复合材料的结构调控及性能研究[J]. 化工学报, 2018, 69(11):4896-4901.
DONG Jinxin, ZHU Zhaoxian, YAO Hongjun, et al. Structure and properties of phenolic aerogel/carbon fiber composites[J]. Chinese Journal of Chemical Engineering and Technology,2018,69(11):4896-4901(in Chinese).
|
[18] |
COX H L. The elasticity and strength of paper and other fibrous materials[J]. British Journal of Applied Physics,1952,3(3):72-79. doi: 10.1088/0508-3443/3/3/302
|
[19] |
FU S Y, LAUKE B. An analytical characterization of the anisotropy of the elastic modulus of misaligned short-fiber-reinforced polymers[J]. Composites Science and Tech-nology,1998,58(12):1961-1972. doi: 10.1016/S0266-3538(98)00033-5
|
[20] |
唐国宏, 陈昌麒. 界面断裂[J]. 复合材料学报, 1994, 11(3):43-49.
TANG Guohong, CHEN Changqi. Interfacial fracture[J]. Acta Materiae Compositae Sinica,1994,11(3):43-49(in Chinese).
|
[21] |
NIE J, XU Y, ZHANG L, et al. Microstructure and tensile behavior of multiply needled C/SiC composite fabricated by chemical vapor infiltration[J]. Journal of Materials Processing Technology,2009,209(1):572-576. doi: 10.1016/j.jmatprotec.2008.02.035
|
[22] |
方光武, 高希光, 陈晶, 等. 加载循环数对2D针刺C/SiC复合材料疲劳剩余强度的影响[J]. 复合材料学报, 2016, 33(1):149-154.
FANG Guangwu, GAO Xiguang, CHEN Jing, et al. Effect of loading cycles on fatigue residual strength of 2D needle punched C/SiC composites[J]. Acta Materiae Compositae Sinica,2016,33(1):149-154(in Chinese).
|
[23] |
邢亚娟, 孙波, 高坤, 等. 航天飞行器热防护系统及防热材料研究现状[J]. 宇航材料工艺, 2018, 48(4):9-15.
XING Yajuan, SUN Bo, GAO Kun, et al. Research status of thermal protection system and thermal protective materials for space vehicle[J]. Aerospace Materials & Technology,2018,48(4):9-15(in Chinese).
|
[24] |
中国国家标准化管理委员会. 纤维增强塑料 拉伸性能试验方法: GB/T 1447—2005[S]. 北京: 中国标准出版社, 2005.
Standardization Administration of the People’s Republic of China. Fiber-reinforced plastic composites-Determination of tensile properties: GB/T 1447—2005[S]. Beijing: Standards Press of China, 2005(in Chinese).
|
[25] |
中国国家标准化管理委员会. 纤维增强塑料 压缩性能试验方法: GB/T 1448—2005[S]. 北京: 中国标准出版社, 2005.
Standardization Administration of the People’s Republic of China. Fiber-reinforced plastic composites-Determination of compressive properties: GB/T 1448—2005[S]. Beijing: Standards Press of China, 2005(in Chinese).
|
[26] |
张冬梅, 叶金蕊, 刘奎, 等. 孔隙微观特征影响CFRP力学性能的细观综述[J]. 复合材料学报, 2013, 30(S1):118-123.
ZHANG Dongmei, YE Jinrui, LIU Kui, et al. Microscopic review of influence of pore microstructure on mechanical properties of CFPR[J]. Acta Materiae Compositae Sinica,2013,30(S1):118-123(in Chinese).
|
[27] |
刘克杰, 朱华兰, 彭涛, 等. 无机特种纤维介绍(一)[J]. 合成纤维, 2013, 42(5):32-37.
LIU Kejie, ZHU Hualan, PENG Tao, et al. The introduction of inorganic special fiber(I)[J]. Synthetic Fiber,2013,42(5):32-37(in Chinese).
|
[28] |
张焱, 祖群. 航空领域用特种高性能玻璃纤维材料[J]. 航空制造技术, 2014, 57(15): 130-131.
ZHANG Yan, ZU Qun. Special high-performance glass fiber materials used in aviation field[J]. Aeronautical Manufacturing Technology, 2014, 57(15): 130-131(in Chinese).
|
[29] |
AVESTON J, COOPER G A, KELLY A. The properties of fiber composites[C]//National Physical Laboratory Conference Proceeding. England: IPS Science & Technology Press, 1971: 1254-1262.
|
[30] |
张盼. 三维针刺C/C复合材料的微结构建模及力学性能预测[D]. 西安: 西北工业大学, 2016.
ZHANG Pan. Microstructure modeling and mechanical properties prediction of three-dimensional needled C/C composites[D]. Xi’an: Northwestern Polytechnical University, 2016(in Chinese).
|