The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor /

Bibliographic Details
Main Authors:	Bozak, Richard F. (Author), Hughes, Christopher E. (Author), Buckley, James (Mechanical engineer) (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2013.
Series:	NASA technical memorandum ; 2013-218066.
Subjects:	Acoustic properties. Aerodynamic noise. Blade tips. Oscillating flow. Pressure ratio. Turbofans. Rotors.
Online Access:	https://purl.fdlp.gov/GPO/gpo49564 http://purl.fdlp.gov/GPO/gpo49564

Description
Item Description:	Title from title screen (viewed June 4, 2014). "August 2013." "Prepared for the Turbo Expo 2013 sponsored by the American Society of Mechanical Engineers (ASME) San Antonio, Texas, June 3-7, 2013." "GT2013-95114."
Physical Description:	1 online resource (8 pages) : illustrations (some color).
Bibliography:	Includes bibliographical references (pages 7-8).