Category Archives: Flow Control

Control of Transitional SBLI The potential of surface morphing techniques, including passive shock control bumps (SCB) and active surface morphing, is explored to control transitional shock wave boundary layer interactions (SWBLI). In addition to reducing the size of the separation bubble, a key objective is to mitigate the low-frequency unsteadiness that can cause detrimental structuralContinue reading “Supersonic flow separation control using surface morphing”