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Aerodynamic analysis of external and internal flows are critical to evaluating performance metrics of aero-propulsion systems. We collaborate with experimental campaigns to improve the utility and applicability of simulation-based analysis to improve the design, predict performance deviations, and identify control strategies for these systems.
Shown here are the RANS and experimental results of a supersonic inlet, focusing on accurately modeling the pressure recovery, mass-capture, separation characteristics, and unsteady effects of shock boundary layer interactions at the ramp-isolator junction.
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