Compressive strength of 24S-T aluminum-alloy flat panels with longitudinal formed hat-section stiffeners having a ratio of stiffener thickness to skin thickness equal to 1.00

Author:	Hickman, William A.
Year:	1947
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-1439
Link:	https://digital.library.unt.edu/ark:/67531/metadc55532/