Calculation of the chordwise load distribution over airfoil sections with plain, split, or serially hinged trailing-edge flaps

Author:	Allen, H. Julian
Year:	1938
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-634
Link:	https://digital.library.unt.edu/ark:/67531/metadc66292/