Cover Image

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
Description
Item Description:Title from title screen (viewed July 9, 2014).
"November 2013."
Physical Description:1 online resource (22 pages) : color illustrations.
Bibliography:Includes bibliographical references (pages 5-6).