CORDIS Project
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This research investigates shock-boundary layer interactions in high-speed aerodynamics. It aims to understand and control the unsteady effects of these interactions to improve the performance of supersonic and hypersonic systems.
Travelling at high speeds entails overcoming adverse effects, such as regions of high heat transfer and surface pressures, unsteady shock waves, and fluid-structure interactions.
The occurrence of shock boundary layer interaction (SBLI) close to the leading edge is common in high-speed intakes.
When accompanied by separation, the interaction adversely affects the performance of the system.
The adverse effects are more than just those related to the energy/efficiency budgets; the separation could…
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