[1] JOACHIM H, MARILYN J S. Hybrid Reynolds-averaged Navier-Stokes/large-eddy simulation closure for separated transitional flows[J]. AIAA Journal, 2017, 55(6):1948-1958. [2] XIAO Z X, CHEN H X, LI Q B, et al. A primary study of transitions in turbulence models[J]. Chinese Journal of Computational Physics, 2006, 23(1):61-65. [3] DURBIN P, WU X. Transition beneath vortical disturbances[J]. Annual Review of Fluid Mechanics, 2007, 39(1):107-128. [4] MICHELASSI V, WISSINK J, FROHLICH J, et al. Large-eddy simulation of flow around low-pressure turbine blade with incoming wakes[J]. AIAA Journal, 2003, 41(11):2143-2156. [5] LIU T X, MA B F. Suitability of low-order numerical schemes in large eddy simulations[J]. Chinese Journal of Computational Physics, 2014, 31(3):307-313. [6] VAN I J. The eN method for transition prediction:Historical review of work at TU Delft[R]. AIAA 2008-3830, Seattle, 2008. [7] KRUMBEIN A, KRIMMELBEIN N, SCHRAUF G. Automatic transition prediction in hybrid flow solver, Part 1:Methodology and sensitivities[J]. Journal of Aircraft, 2009, 46(4):1176-1190. [8] KRIMMELBEIN N, RADESPIEL R. Transition prediction for three-dimensional flows using parallel computation[J]. Computers & Fluids, 2009, 38(1):121-136. [9] BISWAS D, FUKUYAMA Y. Calculation of transitional boundary layers with an improved low-Reynolds-number version of the k-ε turbulence model[J]. Journal of Turbomachinery, 1994, 116(4):765-773. [10] JONES W, LAUNDER J H. The calculation of low-Reynolds-number phenomena with a two-equation model of turbulence[J]. International Journal of Heat and Mass Transfer, 1973, 16(6):1119-1130. [11] WALTERS D K, LEYLEK J H. A new model for boundary-layer transition using a single-point RANS approach[J]. Journal of Turbomachinery, 2004, 126(1):193-202. [12] MENTER F R, LANGTRY R B, LIKKI S R, et al. A correlation based transition model using local variables Part 1:Model formulation[J]. Journal of Turbomachinery, 2006, 128(3):57-67. [13] SPALART P R, ALLMARAS S R. A one-equation turbulence model for aerodynamic flow[J]. Recherche Aeros-patiale, 1992, 439(1):5-21. [14] SHIVAJI M, JAMES D B. Application of the correlation-based γ-Reθt transition model to the Spalart-Allmaras turbulence model[R]. AIAA 2011-3979, Honolulu, 2011. [15] ONUR B, SAMET C C, UNVER K. A novel intermittency distribution based transition model for low-Re number airfoils[R]. AIAA 2013-2531, San Diego, 2013. [16] SAMET C C, ONUR B, UNVER K. A correlation-based algebraic transition model[J]. ARCHIVE Proceedings of the Institution of Mechanical Engineers, Part C:Journal of Mechanical Engineering Science, 2017, 232(21):3915-3929. [17] YOU J Y, KWON O J. Blending of sas and correlation-based transition models for flow simulation at supercritical Reynolds numbers[J]. Computers & Fluids, 2013, 80(1):63-70. [18] 乔磊, 白俊强, 华俊. Gamma-Theta经验转捩模型在DES中的应用[J]. 航空工程进展, 2013, 4(2):226-231. [19] SANCHEZ R M, MENON S. The compressible hybrid RANS/LES formulation using an additive operator[J]. Journal of Computational Physics, 2009, 228(6):2037-2062. [20] 张玉伦, 王光学, 孟德虹, 等. γ-Reθ转捩模型的标定研究[J]. 空气动力学学报, 2011, 29(3):295-301. [21] SPALART P R, DECK S, SHUR M L, et al. A new version of detached-eddy simulation, resistant to ambiguous grid densities[J]. Theoretical and Computational Fluid Dynamics, 2006, 20(3):181-195. [22] DENG F, WU Y Z, LIU X Q. Simulation of vortex in separated flows with DES[J]. Chinese Journal of Computational Physics, 2008, 25(6):683-688. [23] SPALART P R, JOU W H, STRELETS M, et al. Comments on the feasibility of LES for wings, and on a hybrid RANS/LES approach[J]. Advances in DNS/LES, 1997, 1(1):4-8. |