Investigation at large scale of the pressure distribution and flow phenomena over a wing with the leading edge swept back 47.5 degrees having circular-arc airfoil sections and equipped with drooped-nose and plain flaps

Author:	Lange, Roy H.
Additional Authors:	Whittle, Edward F., Jr.
Year:	1949
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L9G15
Link:	https://digital.library.unt.edu/ark:/67531/metadc58279/