An investigation at low speed of a 51.3 degree sweptback semispan wing equipped with 16.7-percent-chord plain flaps and ailerons having various spans and three trailing-edge angles

Author:	Fischel, Jack
Year:	1948
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L8H20
Link:	https://digital.library.unt.edu/ark:/67531/metadc64594/