Separation and Reattachment Fixed Reynolds-Stress Model for Iced Airfoil and Wing Simulations
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Published:2024-09
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Volume:
Page:109587
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ISSN:1270-9638
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Container-title:Aerospace Science and Technology
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language:en
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Short-container-title:Aerospace Science and Technology
Author:
Chen Rong, Wang ShengyeORCID, Wang ShunshunORCID, Cai Jiahong
Reference34 articles.
1. M.C. Xiao, Y.F. Zhang, “Improved Prediction of Flow Around Airfoil Accreted with Horn or Ridge Ice,” AIAA Journal, 59(6): 2318–2327, 2021. https://doi.org/10.2514/1.J059744. 2. F.T. Lynch, A. Khodadoust, “Effects of ice accretions on aircraft aerodynamics,” Progress in Aerospace Sciences, 37(8): 669–767, 2001. https://doi.org/10.1016/S0376-0421(02)00008-8. 3. J.P. Pan, E. Loth, “Reynolds-Averaged Navier–Stokes Simulations of Airfoils and Wings with Ice Shapes,” Journal of Aircraft, 41(4): 879–891, 2004. https://doi.org/10.2514/1.587. 4. C. Marongiu, P.L Vitagliano, G. Zanazzi, et al. “Aerodynamic Analysis of an Iced Airfoil at Medium/High Reynolds Number,” AIAA Journal, 46(10): 2469–2478, 2008. https://doi.org/10.2514/1.34550. 5. X. Chi, Y. Li, H. Chen, et al. “A Comparative Study Using CFD to Predict Iced Airfoil Aerodynamics,” 43rd AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2005-1371, 2005. https://doi.org/10.2514/6.2005-1371.
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