RANS modeling of high-speed aerodynamic flow transition with consideration of stability theory

S Fu, L Wang - Progress in Aerospace Sciences, 2013 - Elsevier
One of the effective approaches to simulate laminar-turbulent transition flows is based on
Reynolds-Averaged Navier–Stokes (RANS) equations. In this review article, the …

Improved k-ω-γ model for crossflow-induced transition prediction in hypersonic flow

L Zhou, R Li, Z Hao, DI Zaripov, C Yan - … Journal of Heat and Mass Transfer, 2017 - Elsevier
Accurate prediction of boundary layer transition is extremely important for the aerodynamic
and aerothermodynamic design of a hypersonic vehicle. Crossflow instability plays a crucial …

[HTML][HTML] 高超声速边界层转捩研究现状与发展趋势

陈坚**, 涂国华, 张毅锋, 徐国亮, 袁先旭, 陈诚 - 2017 - html.rhhz.net
高超声速飞行器边界层容易经历层流/湍流转捩, 层流流动和湍流流动在摩擦阻力, 热交换,
噪声和掺混等方面有巨大差别, 转捩问题已成为制约高超声速技术突破的基础科学问题之一 …

Improvement of transition prediction model in hypersonic boundary layer based on field inversion and machine learning framework

TX Zhang, JQ Chen, FZ Zeng, DG Tang, C Yan - Physics of Fluids, 2023 - pubs.aip.org
The classical four-equation γ− R e θ transition model has presented excellent accuracy in
low-speed boundary layer transition prediction. However, once the incoming flow reaches …

Fully local transition closure model for hypersonic boundary layers considering crossflow effects

L Qiao, J Xu, J Bai, Y Zhang - AIAA Journal, 2021 - arc.aiaa.org
A computational fluid dynamics (CFD) compatible and fully local transition closure model is
proposed for three-dimensional hypersonic boundary layers considering crossflow effects …

Modeling of surface roughness effects on bypass and laminar separation bubble-induced transition for turbomachinery flows

Y Zhang, J Xu, Y Li, L Qiao, J Bai - Physics of Fluids, 2022 - pubs.aip.org
In a previous study, we developed a one-equation transition model for the bypass and
laminar separation bubble (LSB)-induced transition based on local variables. In this paper …

Transition-based constrained large-eddy simulation method with application to an ultrahigh-lift low-pressure turbine cascade flow

X Wang, Z **ao - Journal of Fluid Mechanics, 2022 - cambridge.org
A transition-predictive Reynolds-averaged Navier–Stokes (RANS) model is introduced as
the Reynolds controlling condition to constrained large-eddy simulation (TrCLES) to improve …

Predicting distributed roughness induced transition with a four-equation laminar kinetic energy transition model

Z Liu, Y Zhao, S Chen, C Yan, F Cai - Aerospace Science and Technology, 2020 - Elsevier
A four-equation laminar kinetic energy transition model is developed to predict the
distributed roughness induced transition using local variables. Based on the laminar kinetic …

An improved local correlation-based intermittency transition model appropriate for high-speed flow heat transfer

Z Liu, C Yan, F Cai, J Yu, Y Lu - Aerospace Science and Technology, 2020 - Elsevier
An improved local correlation-based intermittency transition model is developed for high-
speed flow heat transfer in this paper. Based on the intermittency transition model, two …

Parallel compatible transition closure model for high-speed transitional flow

J Xu, J Bai, Z Fu, L Qiao, Y Zhang, J Xu - AIAA Journal, 2017 - arc.aiaa.org
A single-point transition closure model that incorporates analytical results by stability theory
in a reasonably wide range of Mach numbers has been formulated for …