Validation of the predicted circumferential and radial mode sound power levels in the inlet and exhaust ducts of a fan ingesting distorted inflow /

Bibliographic Details

Main Author:	Koch, L. Danielle
Corporate Authors:	AIAA Aeroacoustics Conference, NASA Glenn Research Center
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:	NASA technical memorandum ; 2012-217253.
Subjects:	Sound pressure. Noise reduction. Pressure measurement. Aerodynamic noise. Ducts. Fan blades. Rotors. Cylindrical bodies.
Online Access:	https://purl.fdlp.gov/GPO/gpo26304