Development of an open rotor cycle model in NPSS using a multi-design point approach /

Bibliographic Details

Main Author:	Hendricks, Eric S.
Corporate Authors:	ASME Turbo Expo, NASA Glenn Research Center
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
Series:	NASA technical memorandum ; 2011-217225.
Subjects:	Contrarotating propellers. Turbines. Exhaust emission. Flight envelopes. Propeller blades. Propeller efficiency. Takeoff. Aerodynamics. Fuel consumption.
Online Access:	https://purl.fdlp.gov/GPO/gpo20738