A fuselage addition to increase drag-rise Mach number of subsonic airplanes at lifting conditions

Document details
Author:	Whitcomb, Richard T.
Year:	1958
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-4290
Link:	https://digital.library.unt.edu/ark:/67531/metadc57155/