Updated assessment of an open rotor airplane using an advanced blade design /

Bibliographic Details
Main Author:	Hendricks, Eric S. (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2013.
Series:	NASA technical memorandum ; 2013-218074.
Subjects:	Contrarotating propellers. Fuel consumption. Low noise. Noise intensity. Noise prediction (aircraft) Propulsion system configurations. Propulsion system performance.
Online Access:	https://purl.fdlp.gov/GPO/gpo50523 http://purl.fdlp.gov/GPO/gpo50523

Description
Item Description:	Title from title screen (viewed July 9, 2014). "August 2013." "Prepared for the 49th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE San Jose, California, July 14-17, 2013." "AIAA-2013-3628."
Physical Description:	1 online resource (13 pages) : color illustrations.
Bibliography:	Includes bibliographical references (pages 12-13).