Tests of 2 full℗--scale propellers with different pitch distributions, at blade angles up to 60℗ʻ.

Bibliographic Details
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document eBook
Language:	English
Published:	[Washington] : [s.n.], 1938.
Subjects:	Aeronautics > Research. Airplanes. Engines. Weights and measures.
Online Access:	Electronic resource (PDF)

Description
Item Description:	Contains tables, diagrams, images, and a list references.
Physical Description:	1 online resource (15 pages), digital, PDF file