Effects of Range of Stress and of Special Notches on Fatigue Properties if Aluminum Alloys Suitable for Airplane Propellers.

Bibliographic Details
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document eBook
Language:	English
Published:	[Washington] : [s.n.], 1942.
Subjects:	Aeronautics > Research. Aluminum. Weights and measures.
Online Access:	Electronic resource (PDF)

Description
Item Description:	Includes tables.
Physical Description:	1 online resource (40 pages), digital, PDF file