Effect of leading-edge high-lift devices and split flaps on the maximum-lift and lateral characteristics of a rectangular wing of aspect ratio 3.4 with circular-arc airfoil sections at Reynolds numbers from 2.9 x 10(exp 6) to 8.4 x 10(exp 6)

Author:	Lange, Roy H.
Year:	1948
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L8D30
Link:	https://digital.library.unt.edu/ark:/67531/metadc57702/