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