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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].

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Format:
Book
Government document
Author/Creator:
Hughes, Christopher E., author.
Contributor:
NASA Glenn Research Center, issuing body.
United States. National Aeronautics and Space Administration, sponsoring body.
Series:
NASA technical memorandum ; 2013-214029.
NASA/TM ; 2013-214029
Language:
English
Subjects (All):
Aeroacoustics.
Aerodynamic noise.
Airplanes--Noise.
Airplanes.
Jet planes--Noise.
Jet planes.
Physical Description:
1 online resource (35 pages) : illustrations (some color).
Place of Publication:
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2013.
Notes:
Title from title screen (viewed July 9, 2014).
"December 2013."
Includes bibliographical references (page 13).
"GT2005-68573."
OCLC:
883215359

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