A simplified mathematical model for calculating aerodynamic loading and downwash for wing-fuselage combinations with wings of arbitrary plan form

Author:	Zlotnick, Martin
Year:	1954
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3057
Link:	https://digital.library.unt.edu/ark:/67531/metadc56835/