Flight investigation at Mach numbers from 0.8 to 1.5 to determine the effects of nose bluntness on the total drag of two fin-stabilized bodies of revolution

Author:	Hart, Roger G.
Year:	1955
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3549
Link:	https://digital.library.unt.edu/ark:/67531/metadc57812/