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

An edition of Effect of reduced aft diameter and increased blade number on high-speed counterrotation propeller performance (1989)

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

By Gayle E. Rose

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Publish Date

1989

Publisher

National Aeronautics and Space Administration, Lewis Research Center,For sale by the National Technical Information Service

Language

eng

Pages

Description:

subjects: Aircraft engines, Counter rotation, Counterrotation, Diameters, Propeller blades