The effect of leading-edge droop upon the pressure distribution and aerodynamic loading characteristics of a 45 degree sweptback wing at transonic speeds

Author:	Schmeer, James W
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55I16
Link:	https://digital.library.unt.edu/ark:/67531/metadc61675/