Fuselage-drag tests in the variable-density wind tunnel: streamline bodies of revolution, fineness ratio of 5

Author:	Abbott, Ira H.
Year:	1937
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-614
Link:	https://digital.library.unt.edu/ark:/67531/metadc54304/