[1] 航空工业中国飞机强度研究所. 航空结构强度技术[M]. 北京:航空工业出版社, 2013:357. AVIC Aircraft Strength Research Institute. Aircraft structure strength technology[M]. Beijing:Aviation Industry Press, 2013:357(in Chinese). [2] 冯振宇. 运输类飞机适航要求解读:第二卷结构[M]. 北京:航空工业出版社, 2013:9-20. FENG Z Y. Transport category airplane airworthiness standard interpretation:Vol.2 Structure[M]. Beijing:Aviation Industry Press, 2013:9-20(in Chinese). [3] 强宝平. 飞机结构强度地面试验[M]. 北京:航空工业出版社, 2014:159-162. QIANG B P. Ground testing for aircraft structure[M]. Beijing:Aviation Industry Press, 2014:159-162(in Chinese). [4] 范瑞娟, 王新波, 杨剑锋. 通用飞机全尺寸疲劳试验验证技术[J]. 航空科学技术, 2016, 27(6):57-61. FAN R J, WANG X B, YANG J F. Technique of the full-scale fatigue verification test for general aircraft[J]. Aeronautical Science & Technology, 2016, 27(6):57-61(in Chinese). [5] 吴波, 舒成辉. 基于可靠性准则的飞机结构强度验证方法研究[J]. 航空科学技术, 2016, 27(3):41-45. WU B, SHU C H. Research on certification method for aircraft structural strength based on reliability criterion[J]. Aeronautical Science & Technology, 2016, 27(3):41-45(in Chinese). [6] 薛景川, 薛铁军, 郑旻仲. 原苏联民航飞机耐久性和损伤容限设计与试验技术发展概况[J]. 航空学报, 1993:14(3):A202-A204. XUE J C, XUE T J, ZHENG M Z. The general situation of design and test technique development on civil aircraft durability and damage tolerance of previous USSR[J]. Acta Aeronautica et Astronautic Sinica, 1993, 14(3):A202-A204(in Chinese). [7] 王生楠. 飞机结构设计及强度专业发展研究[C]//航空科学技术学科发展报告. 北京:中国科学技术出版社, 2014:62-83. WANG S N. Advances in aircraft structural design and strength[C]//Report of Advances in Aeronautical Science and Technology. Beijing:China Science and Technology Press, 2014:62-83(in Chinese). [8] 刘兴科, 刘冰, 张建锋. 全尺寸飞机大展弦比机翼静力试验技术研究[J]. 工程与试验, 2014, 54(1):17-21. LIU X K, LIU B, ZHANG J F. Study on static test technology for high-aspect ratio wing of full scale aircraft[J]. Engineering & Test, 2014, 54(1):17-21(in Chinese). [9] 王逾涯, 李岷, 陈群志, 等. 飞机结构静强度与疲劳试验双向加载技术研究[J]. 实验室研究与探索, 2007, 26(11):311-313. WANG Y Y, LI M, CHEN Q Z, et.al. Research on an aircraft structure loading apply technique[J]. Research and Exploration in Laboratory, 2007, 26(11):311-313(in Chinese). [10] 卓轶, 吕媛波, 张文东. 飞机结构强度试验中拉压垫加载技术研究[J]. 科学技术与工程, 2016, 16(2):244-248. ZHUO Y, LV Y B, ZHANG W D. The research of tension/compression pad load technique in structure strength test[J]. Science Technology and Engineering, 2016, 16(2):244-248(in Chinese). [11] 杜星, 冯建民, 贺谦. 全机结构试验起落架随动加载技术研究[J]. 科学技术与工程, 2017, 17(2):288-292. DU X, FENG J M, HE Q. Self-adaptable technique for undercarriage in full scale aircraft structure test[J]. Science Technology and Engineering, 2017, 17(2):288-292(in Chinese). [12] LIU B, ZHANG L, XIA F. Research of weight deduction in full-scale aircraft static strength test[C]//2014 Asia-Pacific International Symposium on Aerospace Technology. Beijing:CSAA, 2014:1-5. [13] 刘冰, 夏峰, 张建峰, 等. 全尺寸飞机静强度试验扣重技术研究[C]//第六届中国航空学会青年科技论坛论文集(上册). 北京:航空工业出版社, 2014:425-429. LIU B, XIA F, ZHANG J F, et al. Research of weight deduct of static test of full scale aircraft[C]//Proceedings of the 6th CSAA Youth Science and Technology Form (Book 1). Beijing:Aviation Industry Press, 2014:425-429(in Chinese). [14] XU Z. Digital simulation of full scale static test of aircraft[J]. Chinese Journal of Aeronautics, 2005, 18(2):138-141. [15] DING Y B, WANG H, CHEN X H, Multi-domain parallel computing for strength analysis of whole aircraft model[J]. Journal of Software Engineering and Applications, 2011, 4(9):546-549. [16] OSTERGAARD M G, IBBOTSON A R, ROUX O L, et al. Virtual testing of aircraft structures[J]. CEAS Aeronautical Journal, 2011, 1(1-4):83. [17] LIN L X, MOU H L, REN J, et al. The static strength reliability analysis of composite aircraft structures[J]. Applied Mechanics and Materials, 2014, 488-489:1215-1218. [18] 牛春匀. 实用飞机结构工程设计[M]. 北京:航空工业出版社, 2008:477-502. NIU C Y. Airframe structural design[M]. Beijing:Aviation Industry Press, 2008:477-502(in Chinese). [19] 孙洁琼. 民用飞机客舱地板横梁结构研究[J]. 民用飞机设计与研究, 2016, 120(1):1-4. SUN J Q. Research on cabin floor cross beam structure for commercial aircraft[J]. Civil Aircraft Design & Research, 2016, 120(1):1-4(in Chinese). [20] 张兆斌, 李明强, 李健. 大型运输机全机静力试验总体规划与实施研究[J]. 航空科学技术, 2015, 26(10):25-27. ZHANG Z B, LI M Q, LI J. Research on comprehensive planning and implementation for full-scale static test of large transporter[J]. Aeronautical Science & Technology, 2015, 26(10):25-27(in Chinese). [21] 谢殿煌, 许光磊. 大型民用飞机全机系统地面综合验证试验平台研究[J]. 航空科学技术, 2015, 26(8):38-42. XIE D H, XU G L. Study on large civil aircraft's all aircraft systems integration verification test platform[J]. Aeronautical Science & Technology, 2015, 26(8):38-42(in Chinese). [22] 王正平, 韩鸿源. 飞机结构试验载荷演算方法研究[J]. 西北工业大学学报, 1999, 17(4):649-652. WANG Z P, HAN H Y. A method for load calculation in aircraft structure test[J]. Journal of Northwestern Polytechnical University, 1999, 17(4):649-652(in Chinese). |