Gas turbine engines having plasma flow-controlled intake systems

摘要: Embodiments of a Gas Turbine Engine (“GTE”) are provided, as embodiments plasma flow-controlled intake system for deployment on GTE. In one embodiment, the GTE includes turbine section, combustion section upstream compressor and section. The plenum, first inlet fluidly coupled to flow-obstructing structure projecting into plenum having an outer surface impinged by airflow directed through during operation A array actuators is disposed and, when activated, suppresses vortex shedding air flowing over structure.