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