Gas turbine inlet fogging system

The present application provides an inlet air fogging system (100) for a gas turbine engine (110). The inlet air fogging system (100) may include a fogging nozzle array (270) and a fogging control system (320) in communication with the fogging nozzle array (270). The fogging control system (320) may include a droplet size measurement system (340) and a humidity level measurement system (390).