Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan /

Bibliographic Details

Main Author:	Hughes, Christopher E. (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Langley Research Center, November 2013.
Series:	NASA technical memorandum ; 2013-216073.
Subjects:	Aircraft performance. Bypass ratio. Fan blades. Fixed wings. Low speed wind tunnels. Noise reduction.
Online Access:	https://purl.fdlp.gov/GPO/gpo50535 http://purl.fdlp.gov/GPO/gpo50535