Theoretical supersonic characteristics of inboard trailing-edge flaps having arbitrary sweep and taper: Mach lines behind flap leading and trailing edges

Author:	Kainer, Julian H.
Year:	1950
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2205
Link:	https://digital.library.unt.edu/ark:/67531/metadc55596/