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

Author:	Dolan, Thomas J.
Year:	1942
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-852
Link:	https://digital.library.unt.edu/ark:/67531/metadc56317/