An exhaust mixer (32) for a gas turbine engine has a plurality of circumferentially distributed alternating inner and outer lobes (42,44), and a plurality of aerodynamic struts (50) positioned and oriented between adjacent inner lobes (42) in the core flow...

An exhaust flow nozzle for a jet engine having a plurality of flow altering components extending from a lip portion of a secondary exhaust nozzle that are movable between first and second positions. In the first position the flow altering components are di...