Open Access
| Issue |
JNWPU
Volume 40, Number 5, October 2022
|
|
|---|---|---|
| Page(s) | 1090 - 1099 | |
| DOI | https://doi.org/10.1051/jnwpu/20224051090 | |
| Published online | 28 November 2022 | |
- 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]
- RAYMER Daniel P. Aircraft design: a conceptual approach[M]. 4th ed. Washington: American Institute of Aeronautics and Astronautics, 1992 [Google Scholar]
- GU Songfen. Overall aircraft design[M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2001 (in Chinese) [Google Scholar]
- 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]
- 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]
- 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]
- 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]
- 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]
- ZHANG Ming. Research on some key technologies of aircraft ground dynamics[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009 (in Chinese) [Google Scholar]
- 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]
- PADOVAN J, KAZEMPOUR A, KIM Y H. Aircraft landing induced tire spinup[J]. Journal of Aircraft, 2015, 28(12): 849–854 [Google Scholar]
- 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]
- 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]
- 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]
- 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]
- 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]
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