Gas turbine engine with aft core driven fan section

A gas turbine engine (20) includes a low spool (3 8) along an engine axis with a forward fan section (22) and a low pressure turbine section (30). A high spool (40) along the engine axis has a high pressure turbine section (28) and an aft core driven fan section (32), the aft core driven fan section (32) axially aft of the high pressure turbine section (28) along the engine axis.