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The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator / Christopher E. Hughes [and three others].

Author
Hughes, Christopher E.
Published
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2013.
Physical Description
1 online resource (35 pages) : illustrations (some color).
Additional Creators
NASA Glenn Research Center and United States. National Aeronautics and Space Administration
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Series
Restrictions on Access
Free-to-read Unrestricted online access
Report Numbers
NAS 1.15:2013-214029
Subject(s)
Note
Title from title screen (viewed July 9, 2014).
"December 2013."
"GT2005-68573."
Bibliography Note
Includes bibliographical references (page 13).
Funding Information
Sponsored by National Aeronautics and Space Administration WBS-22-781-30-75
E-15384
Action Note
committed to retain. Federal Depository Library Program (FDLP). For information on our retention commitment, please contact Microforms and Government Information.
View MARC record | catkey: 12764127