Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods /

Bibliographic Details
Main Author:	Herrick, Gregory Paul, 1972- (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2014.
Series:	NASA technical memorandum ; 2014-218447.
Subjects:	Turbomachinery. Flutter analysis. Inlet flow. Computational fluid dynamics. Aeroelasticity.
Online Access:	https://purl.fdlp.gov/GPO/gpo57922 http://purl.fdlp.gov/GPO/gpo57922

Description
Item Description:	Title from title screen (viewed on June 3, 2015). "December 2014." "Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014."
Physical Description:	1 online resource (17 pages) : color illustrations.
Bibliography:	Includes bibliographical references (pages 15-17).