Open Access
Volume 40, Number 5, October 2022
Page(s) 1090 - 1099
Published online 28 November 2022
  1. NIE Hong, WEI Xiaohui. Key technologies for landing gear of large civil aircrafts[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2008(4): 427–432. [Article] (in Chinese) [Google Scholar]
  2. RAYMER Daniel P. Aircraft design: a conceptual approach[M]. 4th ed. Washington: American Institute of Aeronautics and Astronautics, 1992 [Google Scholar]
  3. GU Songfen. Overall aircraft design[M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2001 (in Chinese) [Google Scholar]
  4. CAO Xin, JIA Yuhong, TIAN Jiajie. Research on landing impact characteristic of multi-wheel bogie landing gear's truck[J]. International Journal of Aerospace System Engineering, 2015, 2(2): 83–86 [Google Scholar]
  5. WANG B, LIN H. Simulation research on multiple wheels and multiple strut aircraft landing gear's kinetic characteristic[J]. Advances in Aeronautical Science and Engineering, 2014, 5(4): 503–507 [Google Scholar]
  6. FAN Hailong. Research on ground loads of aircraft with multi-wheels and multi-landing gear[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2006 (in Chinese) [Google Scholar]
  7. KUANG Aimin, PAN Wenting, FENG Yunwen, et al. Method to calculate load distribution among wheels for the six-wheeled landing gear[J]. Journal of Mechanical Strength, 2009, 31(2): 256–259 (in Chinese) [Google Scholar]
  8. XUAN Jianlin, FENG Yunwen, FENG Yuansheng. Impact of roughness of airport on tricycle-type landing gear wheel load distribution[J]. Acta Aeronautica et Astronautica Sinica, 2009(1): 52–55. [Article] (in Chinese) [Google Scholar]
  9. ZHANG Ming. Research on some key technologies of aircraft ground dynamics[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009 (in Chinese) [Google Scholar]
  10. ZHENG Lan, Nie Hong. MATLAB/simulink based trolley type landing gear landing simulation study[C]//Qingdao 2008 Youth Academic Forum on Simulation Science and Technology, 2008: 49–52 (in Chinese) [Google Scholar]
  11. PADOVAN J, KAZEMPOUR A, KIM Y H. Aircraft landing induced tire spinup[J]. Journal of Aircraft, 2015, 28(12): 849–854 [Google Scholar]
  12. ANSARY M, PANDA G. A sequential quadratic programming method for constrained multi-objective optimization problems[J]. Journal of Applied Mathematics and Computing, 2020 [Google Scholar]
  13. WU W G, XIONG F R, SUN J Q, et al. Dynamic modeling of aircraft landing gear and multi-objective optimization with simple cell mapping method[J]. Transactions of the Canadian Society for Mechanical Engineering, 2018, 43: 80–91 [Google Scholar]
  14. WEI Xiaohui, SONG Xiaochen, NIE Hong, et al. Effect of shock strut flexibility on landing gear shock absorber friction force[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(6): 1604–1611. [Article] (in Chinese) [Google Scholar]
  15. Chief Editorial Committee of aircraft design manual. Aircraft design manual. Volume 9, load, strength and stiffness[M]. Beijing: Aviation Industry Press, 2001 (in Chinese) [Google Scholar]
  16. Commission for Science. Technology and Industry for National Defense. GJB 67.4A-2008. Military Aircraft Strength and Stiffness Specification Part 4: Ground load[S]. GJB 67.4A-2008 (in Chinese) [Google Scholar]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.