Analysis and test evaluation of the dynamic stability of three advanced turboprop models at zero forward speed /

Bibliographic Details

Main Author:	Smith, Arthur F.
Corporate Authors:	Lewis Research Center, United Technologies Corporation. Hamilton Standard Division
Format:	Government Document eBook
Language:	English
Published:	Windsor Locks, Conn. : Cleveland, Ohio : Hamilton Standard Division, United Technologies Corporation ; National Aeronautics and Space Administration, Lewis Research Center, [1985]
Series:	NASA contractor report ; NASA CR-175025.
Subjects:	Dynamic stability. Evaluation. Prop-fan technology. Turboprop engines. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo26015