Open rotor is a next-generation engine architecture being evaluated by NASA in conjunction with Airbus/Boeing and GE/R&R. It has a huge (over 10%) potential fuel burn advantage over conventional turbofan engines. However, the aerodynamic noise from the large, un-ducted fan blades is a concern. We have developed time-linearized RANS based methods in frequency domain to predict tonal noise from open rotors. The common sources are: wake-rotor and vortex-rotor interaction noise. Results from these prediction methods have been validated against data obtained during the recent test campaign run by NASA and GE at the low-speed wind tunnel at NASA Glenn.