Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp

• Published in: Physics of fluids (1994) Vol. 29; no. 12
• Main Authors: Tong, Fulin, Li, Xinliang, Duan, Yanhui, Yu, Changping
• Format: Journal Article
• Language: English
• Published: Melville American Institute of Physics 01.12.2017
• Subjects: Anisotropy; Boundary layer; Compression waves; Computational fluid dynamics; Computer simulation; Curvature; Direct numerical simulation; Fluid dynamics; Fluid flow; Goertler instability; Kinetic energy; Longitude; Longitudinal waves; Mach number; Physics; Reynolds number; Reynolds stress; Spatial data; Stability analysis; Stability criteria; Tensors; Transport equations; Turbulence; Turbulent boundary layer; Velocity distribution; Vorticity
• ISSN: 1070-6631; 1089-7666
• DOI: 10.1063/1.4996762

Numerical investigations on a supersonic turbulent boundary layer over a longitudinal curved compression ramp are conducted using direct numerical simulation for a free stream Mach number M∞ = 2.9 and Reynolds number Reθ = 2300. The total turning angle is 24°, and the concave curvature radius is 15 times the thickness of the incoming turbulent boundary layer. Under the selected conditions, the shock foot is transferred to a fan of the compression wave because of the weaker adverse pressure gradient. The time-averaged flow-field in the curved ramp is statistically attached where the instantaneous flow-field is close to the intermittent transitory detachment state. Studies on coherent vortex structures have shown that large-scale vortex packets are enhanced significantly when the concave curvature is aligned in the spanwise direction. Consistent with findings of previous experiments, the effect of the concave curvature on the logarithmic region of the mean velocity profiles is found to be small. The intensity of the turbulent fluctuations is amplified across the curved ramp. Based on the analysis of the Reynolds stress anisotropy tensor, the evolutions of the turbulence state in the inner and outer layers of the boundary layer are considerably different. The curvature effect on the transport mechanism of the turbulent kinetic energy is studied using the balance analysis of the contributing terms in the transport equation. Furthermore, the Görtler instability in the curved ramp is quantitatively analyzed using a stability criterion. The instantaneous streamwise vorticity confirms the existence of the Görtler-like structures. These structures are characterized by an unsteady motion. In addition, the dynamic mode decomposition analysis of the instantaneous flow field at the spanwise/wall-normal plane reveals that four dynamical relevant modes with performance loss of 16% provide an optimal low-order representation of the essential characteristics of the numerical data. The spatial structures of the dominated low-frequency dynamic modes are found to be similar to that of the Görtler-like vortices.