Results of an advanced fan stage operating over a wide range of speed and bypass ratio /

Bibliographic Details

Main Author:	Suder, Kenneth L. (Kenneth Lee)
Corporate Authors:	Fundamental Aeronautics Program (U.S.) (sponsoring body.), ASME Turbo Expo
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]-[2011]
Series:	NASA technical memorandum ; 216769.
Subjects:	Aerodynamic stalling. Bypass ratio. Computational fluid dynamics. Propulsion system configurations. Transonic compressors. Turbofans. Supersonic speed. Computerized simulation.
Online Access:	https://purl.fdlp.gov/GPO/gpo5211