Engine quieting - Nacelle acoustic treatment

Abstract

This paper describes a major research and development program directed towards reducing the fan noise radiated from the turbofan engines used in current Boeing and McDonnell-Douglas four-engine commercial transports. The reduction in fan noise is expected to be achieved by the modification of the engine nacelles and by the judicious application of acoustically absorptive materials in the fan inlet and discharge ducts. The results of ground tests conducted with full scale acoustically treated nacelles indicate that fan noise reductions on the order of 12 PNdB to 15 PNdB below the noise levels of the current subsonic turbofan engine installations are feasible.