Comprehensive report of fan performance from duct rake instrumentation on 1.294 pressure ratio, 806 ft/sec tip speed turbofan simulator models /

Bibliographic Details

Main Author:	Jeracki, Robert J.
Corporate Author:	NASA Glenn Research Center
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2006]
Series:	NASA technical memorandum ; 213863.
Subjects:	Pressure ratio. Scale models. Simulators. Tip speed. Turbofan engines. Ducted fans. Low speed wind tunnels. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo2965