Open Access
Volume 39, Number 3, June 2021
Page(s) 650 - 659
Published online 09 August 2021
  1. Liiang Jiahua, Bai Junqiang, Li Guojun. Investigation of stall flutter based on peters-ONERA aerodynamic model[J]. Journal of Northwestern Polytechnical University, 2018, 36 (5): 875– 883 [Article][Article](in chinese) [CrossRef] [Google Scholar]
  2. Zhao Jinghui, Yan Wei, Chen Yingchun. Research on stall/spin and anti-spin parachute for large civil aircraft[J]. Flight Dynamic, 2019, 37 (4): 12– 15 [Article](in chinese) [Google Scholar]
  3. Zhao Peng, Yue Hongmei. Stall teaching[J]. Journal of China Civil Aviation Flying College, 2001, 12 (1): 13– 14 [Article](in chinese) [Google Scholar]
  4. Qi Wantao, Li Wei, Lyu Xinbo. Research on flight simulation techniques for the stall and spin characteristics of the airplane[J]. Aeronautical Science & Technology, 2016, 27 (6): 16– 19 [Article](in chinese) [Google Scholar]
  5. Zhang Aiting, Wang Junyang. Research on AC500 aircraftspin flight test[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2007, 39 (1): 113– 116 [Article](in chinese) [Google Scholar]
  6. Li Yongfu, Chen Hong. Wind tunnel technques for studying spin[M]. Beijing: National Defence Industrial Press, 2002: 9– 10(in chinese) [Google Scholar]
  7. Li Xueqin, Gong Xiqin, Jia Xiaopeng. Research on JL8 aircraft stall and spin flight test[J]. Flight Dynamic, 2001, 19 (2): 57– 61 [Article](in chinese) [Google Scholar]
  8. American Society for Testing and Materials. Standard Specification for Design and Performance of a Light Sport Airplane[S]. F2245-11-2011 [Google Scholar]
  9. Li Yadong, Zhang Zijun, Yang Fengtian, et al. Analysis of take-off and climb performance of a certain type of electric aircraft and flighting test[J]. Science Technology and Engineering, 2019, 35: 364– 369 [Article](in chinese) [Google Scholar]
  10. Salanm Abdus, Eunus Zahidul Islam. Recent green aviation technologies an overview[J]. Journal of Modern Science and Technology, 2013, 1 (1): 61– 75 [Article] [Google Scholar]
  11. Jeremy F. Electric motor & power sourceselection for small aircraft propulsion[D]. West Lafayette: Purdue University, 2011 [Google Scholar]
  12. Huang Jun, Yang Fengtian. Development and challenges of electric aircraft with new energies[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37 (1): 57– 68 [Article](in chinese) [Google Scholar]
  13. Zhang Junyao, Tong Gang, Li Yadong. Analysis of take-off acceleration characteristics and simulation model modification of a certain electric aircraft[J]. Advances in Aeronautical Science and Engineering, 2021, 12 (2): 98– 105(in chinese) [Google Scholar]
  14. Liu Chang. Nonlinear flight dynamics at high angle of attack(Ⅰ)[J]. Flight Dynamic, 1989, (2): 97– 99 [Article](in chinese) [Google Scholar]
  15. Rao Qiulei, Han Yixin. High angle of attack aerodynamic modeling and simulation and analysis of stall/spin mode[J]. Chinese Journal of Applied Mechanics, 2018, 35 (3): 472– 477 [Article](in chinese) [Google Scholar]
  16. Chen Yongliang. Nonlinear dynamic characteristics analysis and control of aircraft at high-angle-of-attack[D]. Nanjing: Nanjing University of Aeronautics & Astronautics, 2007: 69–76(in chinese) [Google Scholar]
  17. Li Xiaogang. Analysis and recovery of aircraft's spin characteristics at high angle of attack[D]. Nanjing: Nanjing University of Aeronautics & Astronautics, 2016: 8–9(in chinese) [Google Scholar]
  18. Li Man, Song Bifeng, Jiao Jingshan, et al. Flight dynamics modeling and analysis of high aspect ratio UAV based on flexible beam model[J]. Journal of Northwestern Polytechnical University, 2013, 31 (6): 858– 864 [Article][Article](in chinese) [Google Scholar]
  19. Abramov N B, Goman M G, Khrabrov A N, et al. Simple wings unsteady aerodynamicsat high angles of attack: experimental and modeling results[R]. AIAA-1999-4013 [Google Scholar]
  20. Abramov N B, Goman M G, Greenwell D I, et al. Two-step linear regression method for identification of high incidence unsteady aerodynamic model[R]. AIAA-2001-4080 [Google Scholar]
  21. Wang Qing, Cai Jinshi. Unsteady aerodynamic modeling and identification of airplane at high angles of attack[J]. Acta Aeronautica et Astronautica Sinica, 1996, 17 (4): 391– 398 [Article](in chinese) [Google Scholar]
  22. ZHAO Tao. Research and simulation of high AOA stall/spin and anti-spin parachute[D]. Xi'an: Northwestern Polytechnical University, 2000: 10–12(in chinese) [Google Scholar]
  23. Shi Zhiwei, Huang Da, Wu Genxing, et al. Effects of coupled motion unsteady aerodynamic model on flight characteristics simulation of aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29 (6): 1424– 1427 [Article](in chinese) [Google Scholar]
  24. Jia Rongzhen, Wang Xingren. Modeling and verification of flight simulation system[J]. Flight Dynamics Journal, 1996, 14 (1): 80– 84 [Article](in chinese) [Google Scholar]
  25. Abramov N, Goman M, Khrahrov A. Aircraft dynamics at high incidence flight with account of unsteady aerodynamic effects[R]. AIAA-2004-5274 [Google Scholar]
  26. Gong Zheng. Research on unsteady aerodynamic modeling, control law design and clearance for advanced aerospace vehicle[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2011: 47–55(in chinese) [Google Scholar]
  27. Abramov N, Goman M, Demenkov M, et al. Lateral-directional aircraft dynamics at high incidence flight with account of unsteady aerodynamic effects[R]. AIAA-2005-6331 [Google Scholar]
  28. Cui Yihua, Wang Qi, Li Jikuan. Flight test research of a trainer's spin characteristics[J]. Advances in Aeronautical Science and Engineering, 2012, 3 (1): 16– 18 [Article](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.