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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
Description
Item Description:Title from title screen (viewed on Aug. 6, 2012).
"December, 1985."
Electronic resource.
Physical Description:1 online resource (ix/x, 114 pages) : illustrations
Bibliography:Includes bibliographical references (page 23/24).