Cover Image

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
Description
Item Description:Title from title screen (viewed on Aug. 6, 2012).
"February 2012."
"Prepared for the 17th Aeroacoustics Conference cosponsored by the American Institute of Aeronautics and Astronautics and the Confederation of European Aerospace Societies, Portland, Oregon, June 5-8, 2011."
"AIAA-2011-2808."
Electronic resource.
Physical Description:1 online resource (21 pages) : illustrations (some color).
Bibliography:Includes bibliographical references (page 21).