Numerical study on hypersonic nozzle-inlet starting characteristics in a shock tunnel
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DOI: 10.1016/j.actaastro.2016.10.027
Abstract: Abstract An unsteady viscous numerical simulation is performed to study the starting process of a hypersonic nozzle coupled with a simplified inlet model in a shock tunnel under the condition of inflow Mach number higher… read more here.
Keywords: inlet; shock tunnel; hypersonic nozzle; initial backpressure ... See more keywords