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