The shock corner boundary layer interaction at a freestream Mach number of 3 and a ramp angle of 10° was simulated with four turbulence models: RSM, SA, k-ε, and k-ω SST. Their predictions were compared by examining the shock structure in the symmetry plane, the pressure distribution along the corner line, and the boun...
Xiang-Qian Wu, Rui Yang, Yu-Xin Zhao et al.· Journal of Physics, Conferen...· 0 citations
Shock–bubble interaction constitutes a canonical problem in compressible turbulence, governed by the interplay of compressive and vortical dynamics. Numerical simulations are employed to examine light (He) and heavy (R22) bubbles using dynamic mode decomposition and Favre-weighted turbulent kinetic energy spectra. The...
N. Saigiri, Ribhu Pal, Arnab Roy et al.· The Physics of Fluids· 0 citations
Abstract Content of image described in text. In Hass & Lele (2026 J. Fluid Mech. 1037, A20), we looked at the statistical structure (self-similarity) and entrainment rate of a shear-free turbulent layer bounded by a net zero momentum source layer above and a stable density interface below and found agreement with oscil...
Ryan Hass, S. Lele· Journal of Fluid Mechanics· 0 citations
Stably stratified wall-bounded turbulence governs the dynamics of many environmental and engineering flows. A key challenge is characterizing how stratification modifies mean and turbulent profiles. Monin--Obukhov similarity theory (MOST) is the dominant modelling framework, although it has rarely been rigorously valid...
High-speed turbulent boundary layers govern the transport of momentum, mass, and energy in compressible flows and play a central role in determining aerodynamic performance, skin-friction drag, aerodynamic heating, flow stability, and thermal protection requirements of advanced aerospace vehicles. Over the past three d...
Guillermo Araya, Subhajit Roy, Christian J. Lagares· Applied Sciences· 0 citations
We use cookies to run the site and, with your consent, for analytics and to show ads.
See our Cookie Policy.