Axisymmetric transonic shocks with nonzero angular momentum in divergent nozzles are shown to be stable under small perturbations of the incoming supersonic flow and exit pressure.
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3-D axisymmetric transonic shock solutions of the full Euler system in divergent nozzles
Axisymmetric transonic shocks with nonzero angular momentum in divergent nozzles are shown to be stable under small perturbations of the incoming supersonic flow and exit pressure.