As part of our work in SCRAMJET combustors, we are studying flame behavior, ignition, stabilization, flashback and mode transition in dual mode SCRAMJET combustors both with cavity assisted and strut assisted flame stabilization mechanisms. As part of our work on Combustion Instability prediction and control, we are also looking at vortex driven resonant combustion in Gas Turbine combustors. Active combustion control using secondary injection targeting q' oscillation tailoring are being attempted.
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SCRAMJET Combustion and High Speed Flows
Amardip Ghosh #Advanced Propulsion Systems (APSYS) Lab