Cover Image

Inlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility /

Bibliographic Details
Main Author: Bozak, Richard F. (Author)
Format: Government Document eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2017.
Series:NASA technical memorandum ; 2017-219489.
Subjects:
Acoustic properties.
Aerodynamic characteristics.
Bypass ratio.
Noise reduction.
Rotors.
Turbofan engines.
Online Access:https://purl.fdlp.gov/GPO/gpo82411
http://purl.fdlp.gov/GPO/gpo82411
Description
Item Description:"May 2017."
Physical Description:1 online resource (6 pages) : color illustrations.
Bibliography:Includes bibliographical references (page 2).