Dr. Narayanaswamy recently received a US Air Force grant totaling $371,625 with the Office of Scientific Research. His awarded grant “Investigation of Shock Boundary Layer Interactions to Unravel the Physics of Unstart in Axisymmetric Inlets” is aimed to unlock the physics that govern separated flow dynamics in axisymmetric inlets, which can help towards sensing and controlling inlet unstart. This grant is set to last for 3 years and will be incrementally funded.