Spanwise non-uniform surface temperature creates control streaks that cut high-frequency shear stress by 30% and delay transition for second Mack mode breakdown while reducing peak heat flux for first Mack mode in hypersonic boundary layers.
For this case study this roughly corresponds to𝑘 𝑠 =4, which is the configuration investigated in the previous sections
1 Pith paper cite this work. Polarity classification is still indexing.
1
Pith paper citing it
fields
physics.flu-dyn 1years
2026 1verdicts
UNVERDICTED 1representative citing papers
citing papers explorer
-
Control of deterministic breakdown to turbulence of hypersonic boundary layer with spanwise non-uniform surface temperature
Spanwise non-uniform surface temperature creates control streaks that cut high-frequency shear stress by 30% and delay transition for second Mack mode breakdown while reducing peak heat flux for first Mack mode in hypersonic boundary layers.