A Comparison of the Spanwise Loading Calculated by Various Methods With Experimental Loadings Obtained on a 45 Degree Sweptback Wing of Aspect Ratio 8.02 at a Reynolds Number of 4.0 X 10(6)

Author:	Schneider, William C.
Year:	1951
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-1208
Link:	https://digital.library.unt.edu/ark:/67531/metadc60585/