Ph.D. (Engg) :Studies on the Mixing Layer Between Supersonic Supersonic Co-flows
STC Seminar Hall, Dept. of Aerospace EngineeringTwo supersonic streams merging together in a co-flow configuration are encountered in several engineering systems, such as high-speed propulsion devices and supersonic ejectors. The thin mixing layer that develops between the two streams is dominated by compressibility effects and is prone to shock interactions in shock-dominated flows. The convective Mach number is defined relative to […]