Effect of leading-edge droop on the aerodynamic and loading characteristics of a 4-percent-thick unswept-wing-fuselage combination at transonic speeds

Author:	Schmeer, James W
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L56C14
Link:	https://digital.library.unt.edu/ark:/67531/metadc62188/