The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator /

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, Glenn Research Center, December 2013.
Series:	NASA technical memorandum ; 2013-214029.
Subjects:	Aeroacoustics. Aerodynamic characteristics. Aerodynamic noise. Aircraft noise. Fan blades. Far fields. Laser doppler velocimeters. Low speed wind tunnels.
Online Access:	https://purl.fdlp.gov/GPO/gpo50531 http://purl.fdlp.gov/GPO/gpo50531

Description
Item Description:	Title from title screen (viewed July 9, 2014). "December 2013." "GT2005-68573."
Physical Description:	1 online resource (35 pages) : illustrations (some color).
Bibliography:	Includes bibliographical references (page 13).