2 papers
physics.flu-dyn2026
Control of deterministic breakdown to turbulence of hypersonic boundary layer with spanwise non-uniform surface temperature
L. Boscagli, G. Rigas, P. J. K. Bruce +1
Direct Numerical Simulation (DNS) of a Mach 6 boundary layer over a flat plate is performed to assess the effect of spanwise non-uniform surface temperature on breakdown to turbule…
physics.flu-dyn2026
Stabilisation of second Mack mode in hypersonic boundary layers through spanwise non-uniform surface temperature distribution
L. Boscagli, G. Rigas, O. Marxen +1
The extreme heat fluxes characteristic of hypersonic flows significantly limit the flight envelope of hypersonic vehicles. The role of hydrodynamic instability and the onset of lam…