Nacelle assembly with turbulators

A nacelle assembly for a turbine engine, comprising:

• a cowl for a turbine engine extending along an axis, said cowl extending along an axis and having an exterior surface spaced from an interior surface, said interior surface forming an air inlet for directing air flow to the turbine engine;
• a first turbulator for creating turbulence disposed on said interior surface, said turbulator protruding from said interior surface;
• and
• wherein said interior surface and said exterior surface define a lip, said turbulator located proximate said lip.

A turbine engine assembly, comprising:

• a turbine engine;
• a fan cowl for said turbine engine, said fan cowl extending along an axis and having an exterior surface spaced from an interior surface, said interior surface forming an air inlet for directing air flow to the turbine engine;
• a core cowl extending at least partially about said turbine engine, said fan cowl spaced from said core cowl to define a bypass flow passage;
• and
• a first turbulator for creating turbulence disposed on one of said interior surface and said exterior surface, said turbulator protruding from one of said interior surface and said exterior surface.