Correction of additional span loadings computed by the Weissinger seven-point method for moderately tapered wings of high aspect ratio

Author:	Deyoung, John
Year:	1955
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3500
Link:	https://digital.library.unt.edu/ark:/67531/metadc57484/