Open Access
Volume 38, Number 3, June 2020
Page(s) 580 - 588
Published online 06 August 2020
  1. Li Weiji. Aircraft Preliminary Design[M]. Xi'an: Northwestern Polytechnical University Press, 2004 (in Chinese) [Google Scholar]
  2. Fang Baorui. Aircraft Aerodynamic Layout Design[M]. Beijing: Aviation Industry Press, 1997 (in Chinese) [Google Scholar]
  3. Raymer D P. Aircraft Design:A Conceptual Approach[M]. 5th ed. USA: AIAA Education Series, 2012 [CrossRef] [Google Scholar]
  4. Huang Jun. Aerodynamic Configuration Design of Future Large Aircraft[J]. 航空制造技术, 2010 (19): 26– 29 [Article](in Chinese) [Google Scholar]
  5. Ai Junqiang. Typical High Lift-Drag Ratio Aerodynamic Layout and Development for Aircraft[J]. Aeron autical Science&Technology, 2014 (3): 1– 5 [Article](in Chinese) [Google Scholar]
  6. Zhang Binqian, Wang Yuanyuan, Duan Zhuoyi, et al. Design Method for Large Upswept After Body of Transport Aircraft[J]. Acta Aeronautical et Astronauica Sinica, 2010, 31 (10): 1933– 1939 [Article](in Chinese) [Google Scholar]
  7. Zhang Li, Gao Zhenghong, Du Yiming. Drag Reduction on the Fuselage Shape[C]//The Proceeding of the Asia-Pacific International Symposium on Aerospace Technology, Chengdu, 2018: 376–385 [Google Scholar]
  8. Olaf Brodersen, Simone Crippa, et al. DLR Results From the Fourth AIAA Computational Fluid Dynamics Drag Prediction Workshop[J]. Journal of Aircraft, 2014, 51 (4): 1135– 1147 [Article] [CrossRef] [Google Scholar]
  9. Zhu Ziqiang, Ju Shengjun, Wu Zongcheng. Laminar Flow Active/Passive Control Technology[J]. Acta Aeronautica et Astronautica Sinca, 2016, 37 (7): 2065– 2087 [Article](in Chinese) [Google Scholar]
  10. Zhang Yanzhong. The Development of Aerodynamics & Configuration Technology for Large Aircraft[J]. Engineering Sciences, 2009, 11 (5): 4– 17 [Article](in Chinese) [Google Scholar]
  11. Qiao Zhide. Design of Supercritical Airfoils with Natural Laminar Flow[J]. Experiments and Measurements in Fluid Mechanics, 1998, 12 (4): 24– 29 [Article](in Chinese) [Google Scholar]
  12. Si Liang, Wang Heping, Gong Cuicui. Investigation of Effects of Winglets on Wing's Aerodynamic and Structural Behavior[J]. Acta Aerodynamica Sinica, 2011, 29 (2): 177– 181 [Article](in Chinese) [Google Scholar]
  13. Yang Qingzhen, Zhang Zhongyin. Analysis of the Boundary Layer and Aerodynamic Characteristics of a Supercritical Laminar Wing[J]. Acta Aeronautica et Astronautica Sinca, 2004, 25 (5): 438– 442 [Article](in Chinese) [Google Scholar]
  14. Zhu Ziqiang, Wu Zongcheng, Ding Juchun. Laminar Flow Control Technology and Application[J]. Acta Aeronautica et Astronautica Sinca, 2011, 32 (5): 765– 781 [Article](in Chinese) [Google Scholar]
  15. James G. CODER. Overflow Analysis of the DLR-F11 High-Lift Configuration Including Transition Modeling[J]. Journal of Aircraft, 2015, 52 (4): 1082– 1097 [Article] [CrossRef] [Google Scholar]
  16. Langlois M, Masson C, Paraschivoiu I. Fully Three-Dimensional Transition Prediction on Swept Wings in Transonic Flows– Journal of Aircraft, 1998, 35 (2): 254– 259 [Article] [CrossRef] [Google Scholar]
  17. Langlois M, Masson C, Kafyeke F, Paraschivoiu I. Automated Method for Transition Prediction on Wings in Transonic Flows[J]. Journal of Aircraft, 2002, 39 (3): 460– 468 [Article] [CrossRef] [Google Scholar]
  18. Grabe C, Nie SY, Krumbein A. Transition Transport Modeling for the Prediction of Cross Flow Transition[R]. AIAA-2016-3572 [Google Scholar]
  19. Uwe FEY, Yasuhiro EGAMI, Rolf H. ENGLER. High Reynolds Number Transition Detection by Means of Temperature Sensitive Paint[R]. AIAA-2006-514 [Google Scholar]
  20. Zhang Li, Gao Zhenghong. The Studying of Different Fairings for Fairing and Drag Reduction on the Low-Wing Layout Aircraft[J]. Advances in Aeronautical Science and Engineering, 2018, 9 (2): 197– 202 [Article](in Chinese) [Google Scholar]
  21. Zhang Shengwei, Dong Jianhong, Zhou Lin. Calculating Method Research of Aerodynamic Trim and Trim Expense[J]. Advances in Aeronautical Science and Engineering, 2010, 1 (2): 132– 135 [Article](in Chinese) [Google Scholar]

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