http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan
National Aeronautics and Space Administration,
1 online resource (22 pages) : color illustrations.
Christopher E. Hughes, John A. Gazzaniga.
Title from title screen (viewed July 9, 2014).
Includes bibliographical references (pages 5-6).
Sponsored by National Aeronautics and Space Administration WBS 561581.02.08.03.18.04