TY - JOUR
T1 - Progress in local-variable-based transition-turbulence models for subsonic and transonic boundary layers
AU - XU, Jiakuan
AU - JIANG, Xi
AU - WANG, Yutian
AU - DONG, Ningjuan
AU - QIAO, Lei
AU - BAI, Junqiang
N1 - Publisher Copyright:
© 2025 The Author(s)
PY - 2026/4
Y1 - 2026/4
N2 - The accurate prediction of boundary layer transition represents a persistent and extensively studied challenge in fluid mechanics and aircraft aerodynamic design. It is well recognized that, due to the limitations in computational efficiency and shape complexity, high-resolution numerical simulation techniques and classical stability theory are hard to be applied in the numerical simulation and optimization of complex aircraft designs. The classical correlation-based Langtry and Menter model and laminar kinetic energy model, incorporating stability analysis results, offer efficient solution strategies under the Reynolds-averaged Navier-Stokes framework. Nonetheless, these models rely heavily on the range of available experimental data, which significantly restricts their applicability. Therefore, the Amplification Factor Transport (AFT) transition model anchored in linear stability theory foundations was derived from the findings of Coder and Maughmer and has since been adopted for transition prediction across a variety of complex geometries. This model not only incorporates the analytical foundation of linear stability theory, but also predicts the maximum envelope N value through a transport equation. It enables all non-local variables to be solved locally, ensuring compatibility with massively parallel computational fluid dynamics solvers. This paper systematically introduces the modeling concepts and key variable solution strategies of the currently prevalent transition-turbulence models based on local variables. It emphasizes the evolution of AFT transition frameworks, highlighting their progression from applications in the transition from 2D to 3D compressible boundary layer Tollmien-Schlichting waves, together with the formation of stationary crossflow vortices. In conclusion, this paper addresses the remaining challenges of the amplification factor transport transition model and explores potential directions for its future development.
AB - The accurate prediction of boundary layer transition represents a persistent and extensively studied challenge in fluid mechanics and aircraft aerodynamic design. It is well recognized that, due to the limitations in computational efficiency and shape complexity, high-resolution numerical simulation techniques and classical stability theory are hard to be applied in the numerical simulation and optimization of complex aircraft designs. The classical correlation-based Langtry and Menter model and laminar kinetic energy model, incorporating stability analysis results, offer efficient solution strategies under the Reynolds-averaged Navier-Stokes framework. Nonetheless, these models rely heavily on the range of available experimental data, which significantly restricts their applicability. Therefore, the Amplification Factor Transport (AFT) transition model anchored in linear stability theory foundations was derived from the findings of Coder and Maughmer and has since been adopted for transition prediction across a variety of complex geometries. This model not only incorporates the analytical foundation of linear stability theory, but also predicts the maximum envelope N value through a transport equation. It enables all non-local variables to be solved locally, ensuring compatibility with massively parallel computational fluid dynamics solvers. This paper systematically introduces the modeling concepts and key variable solution strategies of the currently prevalent transition-turbulence models based on local variables. It emphasizes the evolution of AFT transition frameworks, highlighting their progression from applications in the transition from 2D to 3D compressible boundary layer Tollmien-Schlichting waves, together with the formation of stationary crossflow vortices. In conclusion, this paper addresses the remaining challenges of the amplification factor transport transition model and explores potential directions for its future development.
KW - Boundary layer transition
KW - Computational fluid dynamics
KW - Linear stability theory
KW - Local variable
KW - Transition-turbulence model
UR - https://www.scopus.com/pages/publications/105029469330
U2 - 10.1016/j.cja.2025.103688
DO - 10.1016/j.cja.2025.103688
M3 - 文献综述
AN - SCOPUS:105029469330
SN - 1000-9361
VL - 39
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 4
M1 - 103688
ER -