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High-Speed Propulsion
For airbreathing propulsion devices, the challenge is not only generating thrust but maintaining stability and performance across strongly coupled flow, mixing, ignition, and geometric effects. We study ramjets, scramjets, rotating detonation engines, oblique detonation engines, high-speed fuel injection, inlet and combustor interactions, shock-boundary-layer interactions, and propulsion-subsystem coupling.
The central problems are limited residence time, fuel mixing, ignition, shocks, unsteadiness, stability, geometry sensitivity, and coupling across engine components. We use resolved simulations to identify how these mechanisms interact and how they influence device performance.
