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All issues Volume 43 / No 6 (December 2025) JNWPU, 43 6 (2025) 1055-1090 References
Open Access
Issue
JNWPU
Volume 43, Number 6, December 2025
Page(s) 1055 - 1090
DOI https://doi.org/10.1051/jnwpu/20254361055
Published online 02 February 2026
  1. Boeing. Commercial market outlook 2025-2044[EB/OL]. (2025-06-16)[2025-10-18]. https://airinsight.com/airbus-and-boeing-release-20-year-market-forecasts [Google Scholar]
  2. MORRELL P S. Airline finance[M]. 4th ed. London: Ashgate Publishing, 2013: 68–69 [Google Scholar]
  3. SARLIOGLU B, MORRIS C T. More electric aircraft: review, challenges, and opportunities for commercial transport aircraft[J]. IEEE Trans on Transportation Electrification, 2015, 1(1): 54–64 [Article] [Google Scholar]
  4. ZHANG Xuesong, CHEN Yongjun, HU Junling. Recent advances in the development of aerospace materials[J]. Progress in Aerospace Sciences, 2018, 97: 22–34 [Article] [Google Scholar]
  5. DOMINIQUE van den Bossche. The A380 flight control electrohydrostatic actuators, achievements and lessons learnt[C]//25th Congress of International Council of the Aeronautical Sciences, Hamburg, 2006 [Google Scholar]
  6. The House Committee on Transportaion and Infrastructure. Final committee report: the design, development and certification of the Boeing 737 MAX[EB/OL]. (2020-09-01)[2025-10-18]. https://democrats-transportation.house.gov/committee-activity/boeing-737-max-investigation [Google Scholar]
  7. China Aviation Daily. Court hears airplane damage lawsuit between European, Chinese firms[EB/OL]. (2009-01-23)[2025-10-12]. https://www.chinaaviationdaily.com/news/9/9836.html [Google Scholar]
  8. STRVBER H. The aerodynamic design of the A350 XWB-900 high lift system[C]//29th Congress of the International Council of the Aeronautical Sciences, Saint Petersburg, 2014 [Google Scholar]
  9. GILLETTE W. Nacelle installation analysis for subsonic transport aircraft[C]//15th Aerospace Sciences Meeting, Los Angeles, 1977 [Google Scholar]
  10. CHEN A W, TINOCO E N. PAN AIR applications to aero-propulsion integration[J]. Journal of Aircraft, 1984, 21(3): 161–167 [Article] [Google Scholar]
  11. CHEN A W, CURTIN M M, CARLSON R B, et al. TRANAIR applications to engine/airframe integration[J]. Journal of Aircraft, 1990, 27(8): 716–721 [Article] [Google Scholar]
  12. TINOCO E, CHEN A. Transonic CFD applications to engine/airframe integration[C]//22nd Aerospace Sciences Meeting, Reno, 1984 [Google Scholar]
  13. OLIVEIRA G, TRAPP L G, PUPPIN-MACEDO A. Engine-airframe integration methodology for regional jet aircrafts with underwing engines[C]//41st Aerospace Sciences Meeting and Exhibit, Reno, 2003 [Google Scholar]
  14. DEVINE R, CRAWFORD B, BENARD E, et al. A computational investigation of propulsion integration[C]//AIAA 4th Aviation Technology, Integration and Operations(ATIO) Forum, Chicago, 2004 [Google Scholar]
  15. KRENZ G. Transonic configuration design: special course on subsonic/transonic aerodynamic interference for aircraft[R]. AGARD Report 712, 1983 [Google Scholar]
  16. CAMPBELL R L. An approach to constrained aerodynamic design application to airfoils[R]. NAS-TP-3260, 1993 [Google Scholar]
  17. LI W, KRIST S, CAMPBELL R. Transonic airfoil shape optimization in preliminary design environment[J]. Journal of Aircraft, 2006, 43: 639–651 [Article] [Google Scholar]
  18. VAVALLE A, QIN N. Iterative response surface based optimization scheme for transonic airfoil design[J]. Journal of Aircraft, 2007, 44: 365–376 [Article] [CrossRef] [Google Scholar]
  19. ZHANG Yufei. Aerodynamic optimization design of civil passenger aircraft based on advanced CFD methods[D]. Beijing: Tsinghua University, 2010 (in Chinese) [Google Scholar]
  20. LI Runze, ZHANG Yufei, CHEN Haixin. Strategy and method for multi-objective aerodynamic optimization design of supercritical wing[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(5): 165–175 (in Chinese) [Google Scholar]
  21. YANG Kunmiao, ZHANG Weimin. Aerodynamic optimization design of supercritical wing based on wing surface pressure distribution[C]//Proceedings of the 18th Annual Conference of Beijing Society of Theoretical and Applied Mechanics, Beijing, 2012 (in Chinese) [Google Scholar]
  22. KROO I. Drag due to lift: concepts for prediction and reduction[J]. Annual Review of Fluid Mechanics, 2003, 33(1): 587–617 [Google Scholar]
  23. IATA. Aircraft Technology Roadmap to 2050[EB/OL]. (2020-04-10)[2025-10-18]. http://www.innovation4.cn/library/r47258 [Google Scholar]
  24. DENG Yiju, DUAN Zhuoyi, AI Mengqi. Status and development of laminar wing design technology[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(11): 9–25 (in Chinese) [Google Scholar]
  25. YAN Chao. Achievements and predicaments of CFD in aeronautics in past forty years[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(10): 29–65 (in Chinese) [Google Scholar]
  26. SLOTNICK I, KHODADOUST A, ALONSO J, et al. CFD vision 2030 study: a path to revolutionary computational aerosciences[R]. NASA CR 2014-218178, 2014 [Google Scholar]
  27. LEI Juanmian, GUO Mutian, ZHAO Xiaojian, et al. Numerical study of pressure fluctuation spatial and frequency domain characteristics on airfoil surface[J]. Transactions of Beijing Institute of Technology, 2022, 42(8): 834–841 (in Chinese) [Google Scholar]
  28. WU Guanghui, WANG Jing, XIE Hairun, et al. Data- and knowledge-enabled intelligent aerodynamic design for civil aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(5): 43–60 (in Chinese) [Google Scholar]
  29. CHENG Bushi. Aircraft design handbook: volume 4[M]. Beijing: Aviation Industry Press, 2002 (in Chinese) [Google Scholar]
  30. XU Liang, YANG Yi. Study on the sensitivity of aerodynamic performance of civil aircraft to airworthiness noise[J]. Civil Aircraft Design and Research, 2023(3): 129–136 (in Chinese) [Google Scholar]
  31. HENNING Strüber. The aerodynamic design of the A350 XWB-900 high lift system[C]//29th International Congress of the Aeronautical Sciences, Brno, 2014 [Google Scholar]
  32. SUTCLIFFE M, RECKZEH D, FISCHER M. Hicon aerodynamics-high-lift aerodynamic design for the future[C]//25th International Congress of Aeronautical Sciences, Sydney, 2006 [Google Scholar]
  33. LIU Cangsong, LIU Peiqing, MAO Jun, et al. Research on aerodynamic characteristics of AHDF civil aviation aircraft[J]. Aeronautical Computing Technique, 2021, 51(5): 84–86 (in Chinese) [Google Scholar]
  34. LIU C, LUO J. Research on effect of Reynolds number on civil aircraft with ADHF[C]//Interentional Conference on Mechanisms and Robotics, Ghangzhou, 2022 [Google Scholar]
  35. WANG Gang, ZHANG Minghui, MAO Jun, et al. High-lift technology for spoiler on blended-wing-body civil aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(9): 75–91 (in Chinese) [Google Scholar]
  36. RECKZEH D. Aerodynamic design of the high-lift-wing for a megaliner aircraft[J]. Aerospace Science and Technology, 2003, 7(2): 107–119 [Article] [Google Scholar]
  37. CONCILIO ADIMINO I, PECORA R. SARISTU: adaptive trailing edge device(ATED) design process review[J]. Chinese Journal of Aeronautics, 2021, 34(7): 187–210 [Article] [Google Scholar]
  38. NGUYEN N, KAUL U, LEBOFSKY S, et al. Development of variable camber continuous trailing edge flap for performance adaptive aeroelastic wing[C]//SAE AeroTech Congress & Exhibition, Vancouver, 2015 [Google Scholar]
  39. CUMMING S B, SMITH M S, ALI A, et al. Aerodynamic flight test results for the adaptive compliant trailing edge[C]//AIAA Atmospheric Flight Mechanics Conference, 2016 [Google Scholar]
  40. ALBANO E, RODDEN W P. A doublet-lattice method for calculating lift distribution on oscillating surfaces in subsonic flows[J]. AIAA Journal, 1969, 7(2): 68–73 [Google Scholar]
  41. GIESING J P, KALMAN T P, RODDEN W P. Subsonic unsteady aerodynamics for general configurations[C]//10th Aerospace Sciences Meeting, New York, 1972 [Google Scholar]
  42. MORINO L, CHEN L, SUCIU E O. Steady and oscillatory subsonic and supersonic aerodynamics around complex configurations[J]. AIAA Journal, 1975, 13(3): 368–374 [Article] [Google Scholar]
  43. GURUSWAMY G P. Unsteady aerodynamic and aeroelastic calculations for wings using euler equations[J]. AIAA Journal, 1990, 28(3): 461–469 [Article] [Google Scholar]
  44. LEE-RAUSCH E M, BATINA J T. Wing flutter computations using an aerodynamic model based on the navier-stokes equations[J]. Journal of Aircraft, 1996, 33(6): 1139–1147 [Article] [Google Scholar]
  45. BAKER M L, YUAN K A, GOGGIN P J. Calculation of corrections to linear aerodynamic methods for static and dynamic analysis and design[C]//39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, California, 1976 [Google Scholar]
  46. GIESING J P, KALMAN T P, RODDEN W P. Correction factor techniques for improving aerodynamic prediction methods[R]. NASA CR-144967, 1976 [Google Scholar]
  47. JADIC I, HARTLEY D, GIRI J. An enhanced correction factor technique for aerodynamic influence coefficient method[C]//MSC's Proceedings of the 1999 Aerospace User's Conference, 1999 [Google Scholar]
  48. MAO Kun, JING Wuxing, CHENG Pan, et al. A modification to the enhanced correction factor technique for the subsonic wing-body interference model[J]. Aerospace, 2023, 10(1): 40 [Article] [Google Scholar]
  49. ZHANG Hongzhi, ZHOU Qiang, CHEN Gang, et al. Effects of some parameters on the accuracy of aeroelastic proper orthogonal decomposition reduced-order model[J]. Journal of Xi'an Jiaotong University, 2016, 50(11): 104–109 (in Chinese) [Google Scholar]
  50. SHI Yan, WAN Zhiqiang, WU Zhigang, et al. Gust response analysis and verification of elastic aircraft based on nonlinear aerodynamic reduced-order model[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(1): 335–354 (in Chinese) [Google Scholar]
  51. WANG Ziyi. Modeling methods and applications for fluid-solid-thermal coupling in aeroelasticity[D]. Xi'an: Northwestern Polytechnical University, 2021: 41-69 (in Chinese) [Google Scholar]
  52. PATIL M J, HODGES D H, CESNIK C E S. Characterizing the effects of geometrical nonlinearities on aeroelastic behavior of high-aspect-ratio wings[C]//Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, 1999 [Google Scholar]
  53. PATIL M J, HODGES D H, CESNIK C E S. Nonlinear aeroelastic and flight dynamics of high-altitude long-endurance aircraft[C]//40th Structures, Structural Dynamics and Materials Conference, 1999 [Google Scholar]
  54. HUANG Y, TSUSHIMA N, ARIZONO H. Correlation studies of geometrically nonlinear aeroelastic formulations with beam and shell elements[C]//AIAA Science and Technology Forum and Exposition, Orlando, 2020 [Google Scholar]
  55. LIU X, COOK R G, COOPER J E, et al. Static aeroelastic characteristics of a wing including geometric nonlinearities[C]//AIAA Science and Technology Forum and Exposition, San Diego, 2019 [Google Scholar]
  56. ARTOLA M, GOIZUETA N, YNN A, et al. Modal-based nonlinear estimation and control for highly flexible aeroelastic systems[C]//AIAA Science and Technology Forum and Exposition, San Diego, 2020 [Google Scholar]
  57. ARTOLA M, GOIZUETA N, WYNN A, et al. Aeroelastic control and estimation with a minimal nonlinear modal description[J]. AIAA Journal, 2021, 59(7): 2697–2713 [Article] [Google Scholar]
  58. RISO C, DI V F G, RITTER M, et al. A FEM-based approach for nonlinear aeroelastic trim of highly flexible aircraft[C]//International Forum on Aeroelasticity and Structural Dynamics, 2017 [Google Scholar]
  59. RISO C, DI V F G, RITTER M, et al. Nonlinear aeroelastic trim of very flexible aircraft described by detailed models[J]. Journal of Aircraft, 2018, 55(6): 2338–2346 [Article] [Google Scholar]
  60. CAO Qikai, ZENG Huihua, BAI Nan. Identification of aircraft dynamic derivatives based on CFD technology and analysis of reduced frequency[J]. Flight Dynamics, 2011, 29(4): 11–14 (in Chinese) [Google Scholar]
  61. WASZAK M R, SCHMIDT D K. Flight dynamics of aeroelastic vehicles[J]. Journal of Aircraft, 1988, 25(6): 563–571 [Article] [Google Scholar]
  62. SCHMIDT D K, RANEY D L. Modeling and simulation of flexible flight vehicles[J]. Journal of Guidance, Control, and Dynamics, 2001, 24(3): 539–546 [Article] [Google Scholar]
  63. WU Z G, YANG C. Flight loads and dynamics of flexible air vehicles[J]. Chinese Journal of Aeronautics, 2004, 17(1): 17–22 [Article] [Google Scholar]
  64. MARIN P C, POETSCH C. Simulation of flexible aircraft response to gust and turbulence for flight dynamics investigations[C]//AIAA SciTech Forum, 2020 [Google Scholar]
  65. MAO Kun, JING Wuxing, CHEN Shi, et al. Research and verification of rigid-elastic coupling analysis technology for large passenger aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(12): 130972 (in Chinese) [Google Scholar]
  66. SHI Pengfei, TAN Zhiyong, CHEN Jie. Development requirement and design considerations for advanced civil aircraft flight control system[J]. Scientia Sinica Technologica, 2018, 48(3): 237–247 (in Chinese) [Google Scholar]
  67. HUANG Bo, WANG Xinmin, LI Yan. Fly-by-wire control law design of relaxed static stability large civil aircraft[J]. Flight Dynamics, 2010, 28(5): 5 (in Chinese) [Google Scholar]
  68. WAN Zhiqiang, ZHANG Shanshan, WANG Xiaozhe, et al. Maneuver load analysis and alleviation technology of flexible aircraft: review[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(3): 30279 (in Chinese) [Google Scholar]
  69. YANG Chao, QIU Qisheng, ZHOU Yi, et al. Review of aircraft gust alleviation technology[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(10): 527350 (in Chinese) [Google Scholar]
  70. YUAN Zhipeng, XUE Yuan. Research on design and flight test technologies of large aircraft angle-of-attack protection control law[J]. Flight Dynamics, 2020, 38(1): 1–6 (in Chinese) [Google Scholar]
  71. ZHENG Xiaohui, ZHAO Jinghui. Application analysis of high-speed protection on fly-by-wire of commercial aircraft[J]. Civil Aircraft Design and Research, 2014(2): 1–5 (in Chinese) [Google Scholar]
  72. The Boeing Company. Vertical gust suppression system for transport aircraft: United States, US-8774987-B2[P]. 2014-07-08 [Google Scholar]
  73. LIE FA P, Gebre-Egzaibher D. Synthetic air data system[J]. Journal of Aircraft, 2013, 50(4): 1234–1249 [Article] [Google Scholar]
  74. CHEUNG C, SEHGAL S, VALDÉS J J. A machine learning approach to load tracking and usage monitoring for legacy fleets[C]//Proceedings of the 30th Symposium of the International Committee on Aeronautical Fatigue, Krakow, Poland, 2019 [Google Scholar]
  75. O'HIGGINS E, GRAHAM K, DAVERSCHOT D, et al. Machine learning application on aircraft fatigue stress predictions[C]//Proceedings of the 30th Symposium of the International Committee on Aeronautical Fatigue, Poland, 2019 [Google Scholar]
  76. PATIL M J, HODGES D H, CESNIK C E S. Nonlinear aeroelasticity and flight dynamics of high-altitude long-endurance aircraft[J]. Journal of Aircraft, 2001, 38(1): 88–94 [Article] [Google Scholar]
  77. PALACIOS R, CESNIK C. Dynamics of flexible aircraft: coupled flight mechanics, aeroelasticity, and control[M]. Cambridge: Cambridge University Press, 2023 [Google Scholar]
  78. SHI Meng, WANG Yang, WU Zhibin, et al. Study on the anti-crash energy absorption characteristic of composite structure in the sub-cargo compartment[J]. Composites Science and Engineering, 2021(9): 83–88 (in Chinese) [Google Scholar]
  79. ZHOU Wenming. Optimum design and analysis of AD200 fuselage structure for crashworthiness[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2012 (in Chinese) [Google Scholar]
  80. WU Guanghui, ZHANG Zhixiong, WANG Zhaobing, et al. Green and low-carbon development of aviation manufacturing industry[J]. Strategic Study of CAE, 2023, 25(5): 157–164 (in Chinese) [Google Scholar]
  81. HUANG Wen, LIU Xiaoqing, ZHU Jin, et al. Synthesis of maleopimarate and its application as an epoxy curing agent[J]. Chemistry Bulletin, 2011, 74(1): 5 (in Chinese) [Google Scholar]
  82. HUANG Jun, YANG Fengtian. Development and challenges of electric aircraft with new energies[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(1): 12 (in Chinese) [Google Scholar]
  83. DU H Z, ZHANG X, YU H. Design of high-energy-density lithium batteries: liquid to all solid state[J]. Transportation, 2025, 23: 100382 [Google Scholar]
  84. CHAUDHARY R, XU J, XIA Z, et al. Unveiling the multifunctional carbon fiber structural battery[J]. Advanced Materials, 2024, 36(48): 2409725 [Article] [Google Scholar]
  85. BAI Peng, CHEN Qian, XU Guowu, et al. Development status of key technologies and expectation about smart morphing aircraft[J]. Acta Aerodynamica Sinica, 2019, 37(3): 18 (in Chinese) [Google Scholar]
  86. DONG Erbao. Research on realization mechanism and some key technologies of smart morphing aircraft structures[D]. Hefei: University of Science and Technology of China, 2010 (in Chinese) [Google Scholar]
  87. BAI P, LIU X, CHEN Q, et al. Study on dynamic hysteresis and linear modeling of the sliding-skin variable-sweep morphing wing aerodynamics[C]//23rd International Congress of Theoretical and Applied Mechanics, 2012 [Google Scholar]
  88. YANG Junxiang, TIAN Ze, ZHAN Wentao, et al. Research on new generation of distributed IMA core system technology[J]. Microelectronics & Computer, 2019, 36(12): 6 (in Chinese) [Google Scholar]
  89. GASKA T, WERNER B, FLAGG D. Applying virtualization to avionics systems-the integration challenges[C]//Digital Avionics Systems Conference, 2010 [Google Scholar]
  90. JIANG Yin, GAO Shan, TAN Wei, et al. Research on civil aircraft cockpit alarm system based on human factors perspective[J]. Civil Aircraft Design and Research, 2021(1): 85–91 (in Chinese) [Google Scholar]
  91. WATKINS C B, WALTER R. Transitioning from federated avionics architectures to integrated modular avionics[C]//2007 IEEE/AIAA 26th Digital Avionics Systems Conference, Beijing, 2007 [Google Scholar]
  92. ZHAO Chunling, MENG Hua, SUN Liyan. Consideration on the design and integration of commercial aircraft cockpit systems[J]. Avionics Technology, 2023, 54(4): 1–8 (in Chinese) [Google Scholar]
  93. DONG Lei, XIANG Chenyang, ZHAO Changxiao, et al. Comprehensive evaluation of ergonomics of civil aircraft cockpit display-touch control system[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(6): 624053 (in Chinese) [Google Scholar]
  94. WEI Lin, LEI Zhongzhou, QI Meizhao, et al. Construction of 3-D map of aircraft simulated cockpit based on visual SLAM[J]. Civil Aircraft Design and Research, 2023(1): 128–133 (in Chinese) [Google Scholar]
  95. LI Peng, QI Ming. SESAR exploring operations of initial 4D trajectory[J]. International Aviation, 2015(11): 57–58 (in Chinese) [Google Scholar]
  96. 央视网. 我国首次进行四维航迹试验飞行[EB/OL]. (2019-03-20)[2025-10-15]. http://news.cctv.com/2019/03/20/ARTIOpy6BFxStXPJVIxei3yZ190320.shtml?spm=C94212.PV1fmvPpJkJY.S71844.53 [Google Scholar]
  97. CHEN Zhengju. Research of large commercial jet trajectory optimization and 4D navigation[D]. Harbin: Harbin Institute of Technology, 2008 (in Chinese) [Google Scholar]
  98. VILLARROEL J, RODRIGUES L. Optimal control framework for cruise economy mode of flight management systems[J]. Journal of Guidance, Control, and Dynamics, 2016, 39(5): 1022–1033 [Article] [Google Scholar]
  99. VILLARROEL J, RODRIGUES L. An optimal control framework for the climb and descent economy modes of flight management systems[J]. IEEE Trans on Aerospace and Electronic Systems, 2016, 52(3): 1227–1240 [Article] [Google Scholar]
  100. LI Chuang, LIU Xiaoxiong, MA Qingyuan, et al. Four-dimensional descent trajectory optimization for aircraft in turbulence[C]//2016 IEEE International Conference on Information and Automation, Ningbo, 2016: 755-759 [Google Scholar]
  101. ZHANG Zhenxing, YANG Rennong, FANG Yuhuan. LSTM network based on on antlion optimization and its application in flight trajectory prediction[C]//2018 2nd IEEE Advanced Information Management, Communicates, Electronic and Automation Control Conference, 2018: 1658-1662 [Google Scholar]
  102. FENG Tao, LI Hongwei, LI Jiapeng. Analysis of surveillance characteristics and discussion on anti-deception technology of ACAS X[J]. Journal of Xihua University, 2021, 40(6): 39–44 (in Chinese) [Google Scholar]
  103. WANG Fei, YU Chaopeng, XIONG Wei. ADS-B technology overview for the airborne integrated surveillance system[J]. Advances in Aeronautical Science and Engineering, 2024, 15(2): 142–151 (in Chinese) [Google Scholar]
  104. YAN Zhongwu. Research on maneuver load alleviation of large transport aircraft[C]//2nd China Aviation Science & Technology Conference, Beijing, 2015 (in Chinese) [Google Scholar]
  105. WANG Xinhua. Research on realization technique for fly-by-light system[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2012 (in Chinese) [Google Scholar]
  106. COMERFORD D, BRANDT S L, LACHTER J, et al. NASA's single-pilot operations technical interchange meeting: proceedings and findings[R]. NASA/CP-2013-216513, 2013 [Google Scholar]
  107. JIAO Yusong. The development and prospect of hydraulic power system in civil aircrafts[J]. Aeronautical Science & Technology, 2019, 30(12): 1–6 (in Chinese) [Google Scholar]
  108. ZHANG Wanshun, XIE Long, QIAO Yong, et al. Recent advance in foreign aircraft braking technology[J]. Aircraft Design, 2022, 42(6): 43–50 (in Chinese) [Google Scholar]
  109. YE Qiaoling. Research on extremum seeking of optimal slip ratio and anti-skid control of aircraft electric braking system[D]. Changsha: Central South University, 2023 (in Chinese) [Google Scholar]
  110. ZHANG Zhipeng. Research on dynamic characteristics of three-dimensional retracting mechanism of the double struts of main landing gear[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2022 (in Chinese) [Google Scholar]
  111. KNOWLES J A C, KRAUSKOPF B, LOWENBERG M H, et al. Numerical continuation analysis of a dual-sidestay main landing gear mechanism[J]. Journal of Aircraft, 2014, 51(1): 129–143 [Article] [Google Scholar]
  112. YIN Yin. Dynamics and reliability analysis of retraction of landing gear[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2017 (in Chinese) [Google Scholar]
  113. YANG Kai. Effect of mechanical surface strengthening on fatigue behavior of additive manufactured TC18 titanium alloy[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2020 (in Chinese) [Google Scholar]
  114. LI Wei, FIELDING J. Preliminary study of EMA landing gear actuation[C]//Proceedings of the 28th International Congress of the Aeronautical Sciences, Brisbane, Australia, 2012 [Google Scholar]
  115. YAN Yangguang, QIN Haihong, GONG Chunying, et al. More electric aircraft and power electronics[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2014, 46(1): 11–18 (in Chinese) [Google Scholar]
  116. JI Ruiping, LI Weilin, ZHANG Xiaobin, et al. A review of arc fault detection methods for aviation solid-state power controller[J]. Journal of Electrical Engineering, 2015, 10(11): 19–26 (in Chinese) [Google Scholar]
  117. ZHANG Zhuoran, XU Yanwu, YAO Yiming, et al. Electric power system and key technologies of more electric aircraft[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2022, 54(5): 969–984 (in Chinese) [Google Scholar]
  118. SU D, WANG Y, SU D, et al. SCS-Net: a DNN-based electromagnetic shielding effectiveness analysis method for slotted composite structures[J]. Composite Structures, 2023, 313: 116374 [Google Scholar]

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