Flying wing layout has both favorable aerodynamic performance and outstanding radar
scattering characteristics, which is regarded as an ideal stealth aircraft layout. In this paper …

A computational fluid dynamics (CFD) compatible and fully local transition closure model is
proposed for three-dimensional hypersonic boundary layers considering crossflow effects …

An efficient high-fidelity simulation approach is investigated for laminar-to-turbulent
transition in compressible boundary layer flow. This approach combines large-eddy …

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 …

In this study, the suppression of the instability of the hypersonic boundary-layer transition
under thermochemical nonequilibrium (TCNE) using a porous coating configuration is …

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 …

The boundary layer transition process for a straight circular cone with angle of attack (AoA)
of 6° at Mach 6 was studied via high-resolution direct numerical simulations and stability …

The uncertain empirical values of closure coefficients in k–ω–γ transition model flaws the
predictive capability. The current work aims to examine the uncertainty of k–ω–γ transition …

边界层转捩预测一直是流体力学领域的研究热点和难点. 其中, 横流转捩是飞行器表面转捩现象
中关键的一种. 由于受到来流扰动, 壁面粗糙度, 壁面压力梯度, 当地后掠角, 横流特征Reynolds …

The impossibility to reproduce the experimental conditions, which is difficult to perfectly
control and inevitably fluctuate, raises the uncertainties in numerical simulation. The …