Fatigue tests at stresses producing failure in 2 to 10,000 cycles: 24S-T3 and 75S-T6 aluminum-alloy sheet specimens with a theoretical stress-concentration factor of 4.0 subjected to completely reversed axial load

Author:	Hardrath, Herbert F.
Year:	1954
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3132
Link:	https://digital.library.unt.edu/ark:/67531/metadc57149/