Open Access
Issue
JNWPU
Volume 39, Number 4, August 2021
Page(s) 731 - 738
DOI https://doi.org/10.1051/jnwpu/20213940731
Published online 23 September 2021
  1. Lin Guiping, Pu Xueqin, Shen Xiaobin, et al. Icing and anti icing technology for aircraft[M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2016 (in Chinese) [Google Scholar]
  2. Ying Sibin. Study on the theory and methods of aircraft icing tolerant flight control system design[D]. Shanghai: Fudan University, 2010 (in Chinese) [Google Scholar]
  3. Bragg M B, Hutchison T, Merret J. Effect of ice accretion on aircraft flight dynamics[C]//38th Aerospace Sciences Meeting and Exhibit, 2000 [Google Scholar]
  4. Zhang Qiang. Determination method of critical ice shapes for large civil aircraft[J]. Civil Aircraft Design & Research, 2019(1): 53–58 [Article] (in Chinese) [Google Scholar]
  5. Bragg M B, Broeren A P, Blumenthal L A. Iced-airfoil aerodynamics[J]. Progress in Aerospace Sciences, 2005, 41(5): 323–362 [Article] [Google Scholar]
  6. Stebbins S J, Loth E, Broeren A P, et al. Review of computational methods for aerodynamic analysis of iced lifting surfaces[J]. Progress in Aerospace Sciences, 2019, 111: 100583 [Article] [Google Scholar]
  7. Ghisu T, Jarrett J P, Parks G T. Robust design optimization of airfoils with respect to ice accretion[J]. Journal of Aircraft, 2011, 48(1): 287–304 [Article] [Google Scholar]
  8. Jaeggi D M, Parks G T, Kipouros T, et al. The development of a multi-objective tabu search algorithm for continuous optimization problems[J]. European Journal of Operational Research, 2008, 185(3): 1192–1212 [Article] [Google Scholar]
  9. Li H R, Zhang Y F, Chen H X. Optimization of supercritical airfoil considering the ice-accretion effects[J]. AIAA Journal, 2019, 57(11): 4650–4669 [Article] [Google Scholar]
  10. Deng K, Chen H. A hybrid aerodynamic optimization algorithm based on differential evolution and RBF response surface[C]//17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2016 [Google Scholar]
  11. Li Hanghang, Zhou Min. Engineering application of icing detection technique and anti-icing and deicing system on aircraft[J]. Advances in Aeronautical Science and Engineering, 2010(2): 112–115 [Article] (in Chinese) [Google Scholar]
  12. Zhang Jie, Zhou Lei, Zhang Hong, et al. Aircraft icing detection technology[J]. Chinese Journal of Scientific Instrument, 2006, 27(12): 1578–1586 [Article] (in Chinese) [Google Scholar]
  13. Melody J W, Baar T, Perkins W R, et al. Parameter identification for inflight detection and characterization of aircraft icing[J]. Control Engineering Practice, 2000, 8(9): 985–1001 [Article] [Google Scholar]
  14. Ni Zhangsong, Liu Senyun, Wang Qiao, et al. Research progress of test technologies for 3 m×2 m icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(6): 46–53 [Article] (in Chinese) [Google Scholar]
  15. Yi Xian, Gui Yewei, Zhu Guolin. Numerical method of a three-dimensional ice accretion model of aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(11): 2152–2158 [Article] (in Chinese) [Google Scholar]
  16. Stebbins S, Loth E, Broeren A, et al. Aerodynamics of a common research model wing with leading-edge ice shape[J]. Journal of Aircraft, 2021(85): 1–13 [Article] [Google Scholar]
  17. Spalart P R, Jou W, Strelets M et al. Comments on the feasibility of LES for wings and on a hybrid RANS/LES approach[M]. Los Angles, Greyden Press, 1997 [Google Scholar]
  18. Xiao M, Zhang Y. Improved prediction of flow around airfoil accreted with horn or ridge ice[J]. AIAA Journal, 2021(3): 1–10 [Article] [Google Scholar]
  19. Kong Manzhao, Duan Zhuoyi, Ma Yumin. Study on aerodynamic characteristics of ice accretion in different wing span sections[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(2): 32–37 [Article] (in Chinese) [Google Scholar]
  20. Zhao Keliang. Icing calculation, wind tunnel experiment and flight test for large civil aircraft[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2017 (in Chinese) [Google Scholar]
  21. Ratvasky T, Van Zante J. In-flight aerodynamic measurements of an iced horizontal tailplane[C]//37th Aerospace Sciences Meeting and Exhibit, 1999 [Google Scholar]
  22. Hossain K, Sharma V, Bragg M, et al. Envelope protection and control adaptation in icing encounters[C]//41st Aerospace Sciences Meeting and Exhibit, 2003 [Google Scholar]
  23. Ying Sibin, Ai Jianliang. Simulation of aircraft flight envelope protect in icing encounters effects on open loop dynamics[J]. Journal of Sytem Simulation, 2010, 22(10): 2273–2275 [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.