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程小全教授简介
单位：北京航空航天大学航空科学与工程学院飞机系
办公室：北航继教楼207室
电话：010-82338215
邮箱：xiaoquan_cheng@buaa.edu.cn
主要研究方向：
复合材料结构设计技术
复合材料损伤容限分析与设计技术
结构修补技术
结构试验技术
先进飞行器结构设计技术研究等
招生要求：
英语写作和口语表达能力强。
个人经历：
1983-1987 就读于西北工业大学飞行器结构强度专业，获学士学位。
1987-1992 中航二集团第602研究所（即中国直升机设计研究所）升力系统室，主要从事直升机主桨和尾桨的强度设计工作。
1992-1998 北京航空航天大学飞行器设计专业先后获硕士和博士学位。
1998-2000 北京航空材料研究院先进复合材料国防科技重点试验室博士后。
2000-2008 北京航空航天大学飞机设计研究所副教授。
2008.7-现在 北京航空航天大学飞机/直升机设计研究所教授。
2010.9-2011 南昌航空大学飞行器工程学院挂职副院长。
科研经历：
先后承担过科技部国家重大专项、国家863项目、国家自然科学基金、航空科学基金、国防预研基金、国防预研课题等研究工作，以及直-8、直-9、直-10、无人飞机、无人直升机、巡航导弹、战术导弹等多个型号设计分析项目，以及“985工程”学科建设任务。在国内重要学术期刊和国际会议上发表论文230多篇，授权专利10项，教材与专著11部。
近年来发表的论文：
1 Liu Shufeng, Cheng Xiaoquan#, Xu Yunyan, Bao Jianwen, Guo Xin. Study on impact performance of scarf-repaired carbon fiber reinforced polymer laminates [J]. Journal of Reinforced Plastics and Composites, 2015, 34(1): 60―71.
2 徐云研，程小全，张纪奎，郦正能. 复合材料蜂窝夹层结构T型接头拉伸性能研究[J]. 工程力学, 2015, 32(7): 243―248, 256. (Xu Yunyan, Cheng Xiaoquan, Zhang Jikui, Li Zhengneng. Study on composite honeycomb sandwich structure formed T-joints under tensile load [J]. Engineering Mechanics, 2015, 32(7): 243―248, 256.)
3 Wu Pengfei, Cheng Xiaoquan#, Fan Zhou. Buckling performance of composite cylindrical shells subjected to compression loads [C]. 18th International Conference on Composite Structures, 15-18 June, 2015, Lisbon, Portugal.
4 Fan Jingfeng, Cheng Xiaoquan#, Wang Songwei, Guo Xin, Zhang Tao. Experimental and numerical investigation of composite bolted π-joint subjected to bending load [J]. Composites Part B, 2015, 78:324―330.
5 杨曼曼，程小全，胡仁伟. 复合材料开缝柱壳压缩屈曲分析与试验[J]. 高科技纤维与应用, 2015, 40(2): 53―57, 77. (Yang Man-man, Cheng Xiao-quan, Hu Ren-wei. Analysis and experiments of composite cracked cylindrical shell under axial compression [J]. Hi-Tech Fiber & Application, 2015, 40(2): 53―57, 77.)
6 程小全，彭霄婧，胡仁伟，范景峰，刘淑峰. 碳纤维复合材料结构修理用胶粘剂应用研究[J]. 高科技纤维与应用, 2015, 40(5): 11―19. (Cheng Xiao-quan, Peng Xiao-jing, Hu Ren-wei, Fan Jing-feng, Liu Shufeng. A review of the studies on adhesively bonded repair to carbon fiber composite structures [J]. Hi-Tech Fiber & Application, 2015, 40(5): 11―19.)
7 何斌，孟雷，赵军，胡仁伟，程小全. 复合材料旋翼桨叶固有特性和气弹稳定性分析[J]. 高科技纤维与应用, 2015, 40(6): 45―49, 54. (He Bin, Meng Lei, Zhao Jun, Hu Ren-wei, Cheng Xiao-quan. Analysis of natural characteristic and aeroelastic stability with a composite rotor blade [J]. Hi-Tech Fiber & Application, 2015, 40(6): 45―49, 54.)
8 Cheng Xiaoquan#, Fan Jingfeng, Liu Shufeng, Guo Xin, Xu Yahong, Zhang Tao. Design and investigation of composite bolted π-joints with an unconventional configuration under bending load [J]. Composites Part B, 2016, 85:59―67.
9 Liu Peng, Cheng Xiaoquan#, Wang Songwei, Liu Shufeng, Cheng Yujia. Numerical analysis of bearing failure in countersunk composite joints using 3D explicit simulation method [J]. Composite Structures, 2016, 138: 30―39.
10 Liu Shufeng, Cheng Xiaoquan#, Zhang Qian, Zhang Jie, Bao Jianwen, Guo Xin. An investigation of hygrothermal effects on adhesive materials and double lap shear joints of CFRP composite laminates [J]. Composites Part B, 2016, 91:431―440.
11 Wang Songwei, Cheng Xiaoquan#, Guo Xin, Li Xin, Chen Gang. Experimental and finite element analysis of composite to aluminium single lap joints [J]. Experimental Mechanics, 2016, 56: 407―417.
12 Cheng Xiaoquan#, Yang Manman, Zhang Jie, Zhang Qian, Yujia Cheng, Zhang Jikui. Thermal Behavior and Tensile Properties of Composite Joints with Bonded Embedded Metal Plate under Thermal Circumstance [J]. Composites Part B, 2016, 99:340―347.
13 Qian Zhang, Xiaoquan Cheng#, Jie Zhang, Songwei Wang, Yujia Cheng, Tao Zhang. Experimental and numerical investigations of composite box joint under tensile load [J]. Composites Part B, 2016, 107:75―83.
14 Baig, Yasir; Cheng, Xiaoquan#; Hasham, Hasan Junaid; et al. Failure mechanisms of scarf-repaired composite laminates under tensile load [J]. JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING, 2016, 38(7): 2069-2075.
15 刘淑峰，张骞，程小全，李伟东，包建文. 湿热环境下碳纤维复合材料斜面胶接件拉伸试验研究[J]. 高科技纤维与应用, 2016, 41(1): 34―39. (Liu Shu-feng, Zhang Qian, Cheng Xiao-quan, Li Wei-dong, Bao Jian-wen. Tensile performance of adhesively bonded carbon/epoxy composite scarf joints subject to hygrothermal environment [J]. Hi-Tech Fiber & Application, 2016, 41(1): 34―39.)
16 杜晓渊，张婕，程小全，胡仁伟，包建文. 铺层顺序及补片偏转对挖补层合板低速冲击性能的影响[J]. 高科技纤维与应用, 2016, 41(2): 32―37. (DU Xiao-yuan, Zhang Jie, Cheng Xiao-quan, Hu Ren-wei, Bao Jian-wen. Effects of stacking sequence and patch rotation on low-velocity impact properties of scarf-repaired composite laminates [J]. Hi-Tech Fiber & Application, 2016, 41(2): 32―37.)
17 刘鹏，程小全，刘淑峰，王松伟，郭鑫. 沉头单钉连接层合板拉伸试验与分析[J]. 哈尔滨工程大学学报, 2016, 37(6): 782―787. (Liu Peng, Cheng Xiaoquan, Liu Shufeng, Wang Songwei, Guo Xin. Tensile experiment and numerical analysis of single countersunk bolt composite laminate joints [J]. Journal of Harbin Engineering University, 2016, 37(6): 782―787.)
18 张骞，王松伟，马埸浩，张婕，程小全，田春明. 复合材料在现代桥梁工程中的应用[J]. 高科技纤维与应用, 2016, 41(6): 24―30. (ZHANG Qian, WANG Song-wei, MA Yi-hao, ZHANG Jie, CHENG Xiao-quan, TIAN Chun-ming. Application of FRP materials in modern bridge engineering [J]. Hi-Tech Fiber & Application, 2016, 41(6): 24―30.)
19 Cheng Xiaoquan#, Wang Songwei, Zhang Jie, Huang Wenjun, Cheng Yujia, Zhang Jikui. Effect of damage on failure mode of multi-bolt composite joints using failure envelop method [J]. Composite Structures, 2017, 160: 8―15.
20 Cheng Xiaoquan#, Li Xiaoqi, Zhang Jie, Zhang Qian, Cheng Yujia, Zeng Benyin. Evaluation of tensile properties of composite-metal joint with a novel metal insert design by experimental and numerical methods [J]. Chinese Journal of Aeronautics, 2017, 30(3): 1004―1011.
21 Ge Mingming, Cheng Xiaoquan#, Zhang Qian. Compressive test and numerical simulation of center-notched composite laminates with different crack configurations [J]. Polymer Composites, 2017, 38(12): 2631―2641.
22 陈志刚，吴永康，程小全，张涛. 1/3含口盖复合材料柱壳后屈曲性能[J]. 北京航空航天大学学报, 2017, 43(3): 544―550. (Chen Zhigang, Wu Yongkang, Cheng Xiaoquan, Zhang Tao. Post-buckling Performance of 1/3 Composite Cylindrical Shell with Cover [J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(3): 544―550.)
23 张祥林，黄文俊，胡仁伟，张纪奎，程小全.飞行器复合材料结构雷击防护研究进展[J]. 高科技纤维与应用, 2017, 42(4): 8―14. (Zhang Xianglin, Huang Wenjun, Hu Renwei, Zhang Jikui, Cheng Xiaoquan. Investigation progress of lightning protection for aircraft composite structures [J]. Hi-Tech Fiber & Application, 2017, 42(4): 8―14.)
24 熊蕾，胡仁伟，黄文俊，张纪奎，程小全. 复合材料结构热传导与热性能分析研究进展[J]. 高科技纤维与应用, 2017, 42(4): 15―20. (Xiong Lei, Hu Renwei, Huang Wenjun, Zhang Jikui, Cheng Xiaoquan. Research progress on heat transfer analysis and thermal properties of composite structures [J]. Hi-Tech Fiber & Application, 2017, 42(4): 15―20.)
25 沙勐，熊欣，许名瑞，曾本银，郭鑫，程小全. 湿热环境对复合材料疲劳性能的影响[J]. 高科技纤维与应用, 2017, 42(4): 37―43. (Sha Meng, Xiong Xin, Xu Mingrui, Zeng Benyin, Guo Xin, Cheng Xiaoquan. Effect of hygrothermal environment on fatigue properties of composite materials [J]. Hi-Tech Fiber & Application, 2017, 42(4): 37―43.)
26 张羽, 王召娣, 但春明, 黄文俊, 胡仁伟, 程小全. 飞机结构复合材料设计值研究进展[J]. 高科技纤维与应用, 2017, 42(5): 8―15,23. (Zhang Yu, Wang Zhaodi, Dan Chunming, Huang Wenjun, Hu Renwei, Cheng Xiaoquan. Research progress of aircraft composite structural design values [J]. Hi-Tech Fiber & Application, 2017, 42(5): 8―15,23.)
27 Xiaoquan Cheng#, Jie Zhang, JianWen Bao, Benyin Zeng, Yujia, Cheng, Renwei Hu. Low-velocity impact performance and effect factor analysis of scarf-repaired composite laminates [J]. International Journal of Impact Engineering, 2018, 111: 85―93.
28 Xiaoquan Cheng#, Xiaoyuan Du, Jie Zhang, Jikui Zhang, Xin Guo. Effect of stacking sequence and rotation angle of patch on low velocity impact performance of scarf repaired laminates [J]. Composites Part B, 2018, 133: 78―85.
29 Cheng Xiaoquan#, Zhang Jie, Cheng Yujia, Guo Xin, Wu Yongkang, Xu Yahong. Numerical analysis on tensile properties of composite hybrid bolted/bonded joints with flanging [J]. Steel and Composite Structures, 2018, 26(3):265-272.
30 Cheng Xiaoquan#, Liu Shufeng, Zhang Qian, Guo Xin, Bao Jianwen. Hygrothermal effects on mechanical behavior of scarf repaired CFRP laminates subject to axial compression laods: experimental and numerical studies [J]. Polymer Composites, 2018, 39(3):904-914.
31 张婕，程小全，胡仁伟，包建文. 挖补复合材料层合板的拉伸和压缩性能研究现状[J]. 高分子材料科学与工程, 2018, 34(1):178-183.(Zhang Jie, Cheng Xiaoquan, Hu Renwei, Bao Jianwen. Tensile and Compressive Properties of Scarf-Repaired Composite Laminates[J]. Polymer Materials Science and Engineering, 2018, 34(1):178-183)
32 Yihao Ma, Xiaoquan Cheng#, Zhaodi Wang, Xin Guo, Jie Zhang, Yahong Xu. Buckling and post-buckling behaviors of 1/3 composite cylindrical shell with an opening [J]. Steel and Composite Structures, 2018, 27(5):555-566.
33 Qian Zhang, Xiaoquan Cheng#, et al. Investigation of tensile behavior and influence factors of composite-to-metal 2D-scarf bonded joint[J]. Engineering Structures, 2019, 180: 284-294.
34 Xiaoquan Cheng#, Qian Zhang, Jie Zhang, Xin Guo, Zhongrong Niu. Parameters prediction of cohesive zone model for simulating composite/adhesive delamination in hygrothermal environments[J]. Composites Part B, 2019, 166: 710–721.
35 Jikui Zhang, Xianglin Zhang, Xiaoquan Cheng#, Yanwei Hei, Liying Xing, Zhibao Li. Lightning strike damage on the composite laminates with carbon nanotube films: Protection effect and damage mechanism [J]. Composites Part B, 2019, 168: 342―352.
36 Salam Abdus, Xiaoquan Cheng#, Wenjun Huang, Altaf Ahmed, Renwei Hu. Bearing failure and influence factors analysis of metao-to-composite bolted joints at high temperature[J]. Journal of the Brazilian Society of Mechanical Science and Engineering, 2019, 41: 298.
37 Salam Abdus, Xiaoquan Cheng#, Yujia Cheng, Renwei Hu, Abid Muhammad. Dynamic properties of single and muti-bolted compoaite joints at different bolt-loads and elevated temperature[J]. Australian Jounnal of Mechanical Engineering, 2019, DOI: 10.1080/14484846.2019. 1629188.
38 陈坤，舒茂盛，胡仁伟，郭鑫，程羽佳，程小全#. 带衬套沉头螺栓复合材料/金属接头拉伸性能[J]. 北京航空航天大学学报, 2019, 45(3): 633―640. (Chen Kun, Shu Maosheng, Hu Renwei, Guo Xin, Cheng Yujia, Cheng Xiaoquan. Tensile performance of countersunk bolted composite/metal joints with sleeve [J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(3): 633―640.)
39 邓金鑫，陈少军，张羽，黄文俊，程小全#. 复合材料设计、分析和工艺软件发展现状[J]. 高科技纤维与应用, 2019, (3): 42―51. (Deng Jinxin, Chen Shaojun, Zhang Yu, Huang Wenjun, Cheng Xiaoquan. Development of composite structural design, analysis and manufacturing software [J]. Hi-Tech Fiber & Application, 2019, (3): 42―51.)
40 Jie Zhang, Xiaoquan Cheng#, Xin Guo, Jianwen Bao, Wenjun Huang. Effect of environment conditions on adhesive properties and material selection in composite bonded joints [J]. International Journal of Adhesion and Adhesives, 2020, 96: 102302.
41 Xiaoqi Li, Xiaoquan Chenga#, Xin Guo, Shufeng Liu, Zhiyong Wang. Tensile properties of a hybrid bonded/bolted joint: Parameter study[J]. Composite Structures, 2020, 245:112329.
42 Yihao Ma, Xiaoquan Cheng#, Jikui Zhang, Dafang Zhao, Wenjun Huang. Prediction of resin pocket geometry around rigid fiber inclusion in composite laminate by hot-pressing of prepregs [J]. Journal of Composite Materials, 2020, 54(15): 1987-1999.
43 Du Xiaoyuan, Cheng Xiaoquan#, Cheng Yujia, Huang Wenjun, Chen Gang. Analysis and design improvement of composite bolted Π-joints under bending load [J]. Journal of the Brazilian Society of Mechanical Science and Engineering, 2020, 42: 384.
44 Jie Zhang, Xiaoquan Cheng#, Yujia Cheng, Xin Guo, Liu Yang. Effect of over-ply on moisture absorption behavior of scarf-repaired composite laminate [J]. International Journal of Adhesion and Adhesives, 2020, 102: 102683.
45 张婕，程小全#，程羽佳，冯振宇. 湿热环境对CCF800/环氧挖补板拉压性能的影响[J]. 北京航空航天大学学报, 2020, 46(6): 1116-1124. (Zhang Jie, Cheng Xiaoquan, Cheng Yujia, Feng Zhenyu. Effect of hygrothermal environment on tensile and compressive properties of CCF800/epoxy scarf-repaired laminates [J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(6): 1116-1124.)
46 周震，程小全#，张涛，陈磊，吴永康. 可收卷复合材料层板大变形弯曲性能研究[J]. 工程力学, 2020, 37(8):213-220, 229. (Zhou Zheng, Cheng Xiaoquan, Zhang Tao, Chen lei, Wu Yongkang. Study on large deformation bending properties of rollable composite laminates [J]. Eigneering Mechanics, 2020, 37(8):213-220, 229.)
47 Jie Zhang, Xiaoquan Cheng#, Jikui Zhang, Xin Guo, Wenjun Huang. Effect of curing condition on bonding quality of scarf-repaired composite laminates [J]. Chinese Journal of Aeronautics, 2020, 33(8): 2257-2267.
48 杜晓渊，程小全#，王志勇，胡仁伟. 碳纤维复合材料回收与再利用技术进展[J]. 高分子材料科学与工程, 2020, 36(8): 182-190. (Du Xiaoyuan, Cheng Xiaoquan, Wang Zhiyong, Hu Renwei. Recycling and reusing of carbon fiber reinforced polymer: a current technical progress [J]. Polymer Materials Science and Engineering, 2020, 36(8): 182-190.)
49 Cheng Xiaoquan#, Zhang Jie, Cheng Yujia, Guo Xin and Huang Wenjun Huang. Effect of curing condition on mechanical properties of scarf-repaired composite laminates[J]. Steel and Composite Structures, 2020, 37(4): 419-429.
50 Xiangli Zhang, Jikui Zhang, Xiaoquan Cheng#, Wenjun Huang. Carbon nanotube protected composite laminate subjected to lightning strike: interlaminar film distribution investigation [J]. Chinese Journal of Aeronautics, 2021, 34(2): 620-628.
51 Xiaoqi Li, Xiaoquan Cheng#, Yujia Cheng, Zhiyong Wang, Wenjun Huang. Study on tensile propertiesof a composite-metal single-lap hybrid bonded/bolted joint [J]. Chinese Journal of Aeronautics, 2020, 34(2): 629-640.
52 Mingming Ge, Xiaoquan Cheng#, Wenjun Huang, Renwei Hu, Yujia Cheng. Damage mode and load distribution of countersunk bolted composite joints [J]. Journal of Composite Materials, 2021, 55(13): 1717-1732.
53 程小全.飞机结构设计课程教学目标探讨[J].力学与实践, 2021, 43(3): 453-356. (Cheng Xiaoquan. The objectives of aircraft structure design course. Mechanics in Engineering, 2021, 43(3): 453-456.)【教学研究】
54 Cheng Xiaoquan, Du Xiaoyuan, Chen Kun, Shu Maosheng, Liu Xiaodong, Chen Gang. Tensile performances of single-lap countersunk composite joints with metallic bushing[J]. Steel and Composite Structures, 2021, 40(3): 421-434.
55 程小全#, 杜晓渊. 纤维增强复合材料疲劳寿命预测及损伤分析模型研究进展[J]. 北京航空航天大学学报, 2021, 47(7): 1311-1322. (Cheng Xiaoquan, Du Xiaoyuan. Development of fatigue life prediction and damage modeling of fiber-reinforced composite [J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(7): 1311-1322.)
56 张祥林,孟庆春,许名瑞,曾本银,程小全,孙炜. 吸湿后碳纤维复合材料正交层合板拉伸疲劳性能[J]. 材料工程,2021, 49(8): 169-177. (Zhang Xianglin, Meng Qingchun, Xu Mingrui, Zeng Benyin, Cheng Xiaoquan#, Sun Wei. Tensile fatigue properties of carbon fiber reinforced composite orthogonal laminates after moisture absorption [J]. Journal of Materials Engineering, 2021, 49(8): 169-177.)
57 程小全,张纪奎,郦正能.飞机结构设计中载荷安全系数的工程意义[J].力学与实践, 2021, 43(4): 599-602. (Cheng Xiaoquan, Zhang Jikui, Li Zhengneng. Engineering application of load safety factor in aircraft structure design[J]. Mechanics in Engineering, 2021, 43(4): 599-602.)【教学研究】
58 陈琨,张祥林,安子乾,程羽佳,程小全,冯振宇.温度对碳纤维平纹布正交层合板拉伸疲劳性能的影响[J].材料导报, 2021, 35(16): 16195-16200. (Chen Kun, Zhang Xianglin, An Ziqian, Cheng Yujia, Cheng Xiaoquan, Feng Zhenyu. Effect of temperature on fatigue properites of carbon fiber orthogonal composite laminates[J]. Materials Reports, 2021, 35(16): 16195-16200.)
59 张纪奎,秦绍成,程小全,郦正能.增材制造技术发展对飞机结构设计教学的影响[J].力学与实践, 2021, 43(5): 760-765. (Zhang Jikui, Qin Shaocheng, Cheng Xiaoquan, Li Zhengneng. Influence of additive manufacturing technology development on aircraft structure[J]. Mechanics in Engineering, 2021, 43(5): 760-765.)【教学研究】
60 安子乾，舒茂盛，程羽佳，郭鑫，刘小冬，程小全. 3钉带衬套复合材料/金属接头拉伸疲劳性能试验研究[J]. 材料导报,2021, 35(20): 20081-20086.（An Ziqian, Shu Maosheng, Cheng Yujia, Guo Xin, Liu Xiaodong, Cheng Xiaoquan. Experimental Study on tensile fatigue properties of composite/metal bolted joints with 3-pin and sleeves[J]. Materials Reports, 2021, 35(20): 20081-20086.）
61 安子乾，舒茂盛，程羽佳，郭鑫，程小全.3钉带衬套复合材料/金属接头拉伸疲劳性能[J]. 材料工程,2021, 49(12): 164-174.（An Ziqian, Shu Maosheng, Cheng Yujia, Guo Xin, Cheng Xiaoquan. Tensile fatigue properties of composite/metal bolted joints with 3-pin and sleeves[J]. Journal of Materials Engineering, 2021, 49(12): 164-174.）
62 Xu, Mingrui; Zeng, Benyin.; An, Ziqian; Xiong, Xin; Cheng, Xiaoquan. Experimental and Numerical Investigation on Fatigue Properties of Carbon Fiber Cross-Ply Laminates in Hygrothermal Environments [J]. Polymers, 2022, 14, 1857.
63 Zhuang, Q.; Yue, P.; Li, K.; Guo, X.; Cheng, X. Study on Low-Velocity Impact Performance of Coal-Based Carbon Foam Sandwich Structures in Thermal Protection Systems. Aerospace, 2023, 10, 630.
64 Zhuang, Q.; Cheng, X.; Yue, P.; Guo, X.; Li, K. Study on Failure Criteria and the Numerical Simulation Method of a Coal-Based Carbon Foam under Multiaxial Loading. Aerospace, 2023, 10, 721.
65 邓金鑫，陈林，卢思彤，侯育欣，黄文俊，程小全．某型飞机复合材料结构 损伤分布规律[J/OL]．北京航空航天大学学报. 50(3): 920-930. (DENG J X， CHEN L， LU S T， et al. Damage distribution of composite structures of a certain type aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50(3):920-930)
66 冉广陵，马埸浩，安子乾，赵大方，郭鑫，程小全．含不同直径微脉管层合 板拉伸性能研究[J/OL]．北京航空航天大学学报. https://doi.org/10.13700/j.bh.1001-5965.2022.0490
67 薛茜薇，杜晓渊，郭鑫，程羽佳，程小全．沉头螺接复合材料接头失效预测 强度包线法[J/OL]．工程力学. https://kns.cnki.net/kcms/detail/11.2595.o3.20221107.1413.008.html
68 程小全，蔡墨泉，王松伟．飞机可动翼面缝隙封严结构研究进展[J/OL]．北京 航空航天大学学报. https://doi.org/10.13700/j.bh.1001-5965.2023.0397
69 An, Z.; Cheng, X.#; Zhao, D.; Ma, Y.; Guo, X.; Cheng, Y. Tensile and Compressive Properties of Woven Fabric Carbon Fiber-Reinforced Polymer Laminates Containing Three-Dimensional Microvascular Channels[J]. Polymers, 2024, 16, 665.
70 Zhang, T.; Luo, Z.; Li, K.; Cheng, X#. Experimental and Numerical Investigation of Prepreg-RTM Co-Curing Molding Composite Bolted T-Joint under Bending Load. Polymers, 2024, 16, 1018. https://doi.org/10.3390/polym 16071018.
发行的标准
1. 王玉梅，徐樑华，顾轶卓，李磊，李德利，沈真，李常清，陈利，程小全等. GB/T 40724-2021 碳纤维及其复合材料术语. 国家市场监督管理总局/国家标准化管理委员会 发布，2022-05-01 实施。
授权的专利
1. 武鹏飞，程小全，郭鑫，王松伟，刘淑峰. 自动升降公路减速带(发明专利号：ZL 2014 1 0816654.1). 授权公开（公告）号：CN104594244B，授权公开（公告）日: 2017.01.04.
2. 武鹏飞，程小全，郭鑫，刘淑峰，王松伟. 冲击试验机(发明专利号：ZL 2013 1 0744438.6). 授权公开（公告）号：CN103712765B，授权公开（公告）日: 2015.12.30.
3. 张涛，王国勇，张东华，程小全，许亚洪，柯红军，李丽英. 一种复合材料π型耳片式接头及其整体共固化成型方法(发明专利号：ZL2013 10478819.4). 授权公开（公告）号：CN103538715B，授权公开（公告）日: 2016.06.08.
4. 李成虎，武哲，程小全，殷实，刘丽莎. 一种蒙皮加筋圆柱壳结构的试验夹具与典型试件(发明专利号：ZL2013 107117416). 授权公开（公告）号：CN103639941B, 授权公开（公告）日: 2015.06.10.
5. 李成虎，武哲，程小全，殷实，刘丽莎. 一种蒙皮加筋圆柱壳结构的试验夹具(实用新型专利号：ZL2013208491233). 授权公开（公告）号：CN203765492U, 授权公开（公告）日: 2014.08.13.
6. 程小全，张骞，王松伟，郭鑫. 一种纤维增强复合材料飞行器舱段连接结构及其制备方法(发明专利号：ZL 2017 1 1014578.2). 授权公告号：CN 108032988 B, 授权公告日: 2020.06.16.
7. 程小全，庄淇凯，张婕，程羽佳，吴永康. 一种可用于疲劳试验机的空气冷却热防护结构(发明专利号：ZL 2018 1 0994427.6). 授权公告号：CN 109060510 B, 授权公告日: 2021.02.02.
8. 程小全，周震，郭鑫，程羽佳，吴永康. 一种应用于位移加载的三点弯疲劳试验装置(发明专利号：ZL 2019 1 1367328.6). 授权公告号：CN 109060510 B, 授权公告日: 2021.03.08.
9. 程小全，庄淇凯. 一种基于碳泡沫的夹层结构及其制备方法和维修方法(发明专利号：ZL 2021 1 1081463.1). 授权公告号：CN 113771445 B, 授权公告日: 2022.11.01.
10. 程小全，庄淇凯. 一种基于树脂基碳泡沫的隔热瓦及其制备方法(发明专利号：ZL 2021 1 1082915.8). 授权公告号：CN 113669558 B, 授权公告日: 2023.03.14.
11. 程小全，杜晓渊. 一种复合材料螺栓连接结构的强度和失效模式的预测方法（发明专利：ZL 2021 1 1043981.4). 授权公告号：CN 1113722861 B, 授权公告日: 2023.07.18.
12. 程小全，李浩东等. 一种用于冲击分离试验的试验系统（发明专利：ZL 2022 1 0264337.8）.授权公告号：CN 1100114150 B, 授权公告日: 2023.11.10.
出版的教材与著作
1. 贾玉红, 程小全主编.《现代民用飞机结构与系统》. 北京：北京航空航天大学讲义，2004.1.
2. 郦正能主编.《飞行器结构学》. 北京: 北京航空航天大学出版社, 2005.1（获2006年北京高等教育精品教材称号，国家教委重点教材）.
3. 郦正能主编, 程小全副主编.《飞机部件与系统设计》. 北京: 北京航空航天大学出版社, 2006.5（国防重点教材）（获2008年获北京高等教育精品教材称号）.
4. 高振荣主编，程小全、薛忠民副主编.《英汉复合材料技术词汇》. 北京：化学工业出版社，2007. 01.
5. 程小全译，Michael, C.Y. Niu著.《实用飞机结构工程设计》. 北京：航空工业出版社，2008.10（获航空科技图书出版专项资助）.
6. 冯振宇，程小全，张纪奎译. Michael, C.Y. Niu著.《实用飞机结构应力分析与尺寸设计》. 北京：航空工业出版社，2009.12（获航空科技图书出版专项资助）.
7. 郦正能主编，程小全等副主编.《飞行器结构学（第2版）》. 北京: 北京航空航天大学出版社, 2010.03（普通高等教育“十一五”国家级规划教材，2011年11月获教育部2011年普通高等教育精品教材）.
8. 程小全，张纪奎译. Michael, C.Y. Niu著.《实用飞机复合材料结构设计与制造》. 北京：航空工业出版社，2010.11.
9. 范金娟，程小全，陶春虎编著.《聚合物基复合材料构件失效分析基础》. 北京：国防工业出版社，2011.06（获国防科技图书出版基金资助）.
10. 范金娟，程小全等译，[美]L.A. Carlsson, G.A. Kardomateas著.《夹层复合材料结构与失效机制》. 北京: 国防工业出版社，2019.
11. 郦正能，程小全等著.《飞机部件与系统设计（第2版）》.北京：北京航空航天大学出版社，2021.01(教育部高等学校航空航天类专业教学指导委员会推荐教材).
12. 程小全主编，程小全, 张纪奎, 贾玉红 等.《飞行器结构学（第3版）》. 北京：京航空航天大学出版社，2023.05(工业和信息化部“十四五”规划教材、普通高等教育“十一五”国家级规划教材、北京高等教育精品教材).
教育理念：
学生是教师的未来，教育真正能够帮助的是那些想提升自己的人。
《飞机结构设计》北航学堂MOOC课程链接：http://mooc.buaa.edu.cn/courses/course-v1:BUAA+BUAA_FG+2019_T2/about
《飞机结构设计》中国大学MOOC课程链接：https://www.icourse163.org/course/BUAA-1464040178?from=searchPage
《飞机结构设计》学习强国平台课程链接：https://www.xuexi.cn/lgpage/detail/index.html?id=2466700361203482499
《飞机结构设计-专业技能提升》工信人才教育服务平台链接：https://cms.wling.cn/GongXin/CourseShow/43741?module=4
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http://graduate.buaa.edu.cn/TutorInfo.jsp?id=14863
北京航空航天大学 飞行器设计 博士研究生毕业 博士学位 硕博连读，硕士导师寇长河，博士导师郦正能。博士论文研究复合材料层合板和夹层板低速冲击及冲击后压缩性能。
西北工业大学 飞机结构强度 大学本科毕业 学士学位 主要学习飞机结构强度分析与设计技术
北京航空航天大学 航空科学与工程学院 教授 教学科研 从事飞行器结构设计与分析教学、科研工作
北京航空材料研究院 先进复合材料国防重点实验室 博士后 博士后 复合材料性能表征
中国直升机设计研究所 升力系统室 室工会主席 工程师 直升机旋翼设计 直-8、直-11桨叶设计分析
国际竹藤中心第四届学术委员会委员
[2]. 2021.5 -- 2026.5中国复合材料工业协会先进复合材料专业委员会副主任委员
[3]. 2021.4 -- 2025.4中国复合材料工业协会专家库专家
[4]. 2014.10 -- 至今中国航空学会失效分会非金属失效分析专业委员
[5]. 2018.3 -- 至今CSTM中国材料与试验团体标准委员会航材领域委员会委员
[6]. 2018.5 -- 至今中国航空工业集团公司/中国航空发动机集团有限公司物理冶金人员资格鉴定委员会委员
[7]. 2020.10 -- 至今河北省航空螺旋桨结构与动力性能重点实验室第一届学术委员会委员
