The effect of inlet installation on the zero-lift drag of a 60 degree delta-wing-body configuration from flight tests at Mach numbers from 0.8 to 1.86

Author:	Merlet, Charles F.
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55I09
Link:	https://digital.library.unt.edu/ark:/67531/metadc61586/