Investigation of the Laminar Aerodynamic Heat-Transfer Characteristics of a Hemisphere-Cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8

Author:	Crawford, Davis H.
Year:	1956
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-1323
Link:	https://digital.library.unt.edu/ark:/67531/metadc60724/