Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps

Author:	Sivells, James C.
Year:	1947
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-942
Link:	https://digital.library.unt.edu/ark:/67531/metadc60264/