Effect of reduced aft diameter and increased blade number on high-speed counterrotation propeller performance /

Bibliographic Details
Main Author:	Rose, Gayle E.
Corporate Author:	Lewis Research Center
Other Authors:	Jeracki, Robert J.
Format:	Government Document Book
Language:	English
Published:	[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [1989]
Series:	NASA technical memorandum ; 102077.
Subjects:	Aircraft engines. Counterrotation. Diameters. Propeller blades.
Online Access:	https://purl.fdlp.gov/GPO/LPS61130

Description
Item Description:	Microform.
Physical Description:	1 volume Also available via Internet from the NASA Technical Report Server web site. Address as of 6/23/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900004036%5F1990004036.pdf; current access is available via PURL.