Measurements of Aerodynamic Heat Transfer and Boundary-Layer Transition on a 10 Degree Cone in Free Flight at Supersonic Mach Numbers Up to 5.9

Author:	Rumsey, Charles B.
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L56B07
Link:	https://digital.library.unt.edu/ark:/67531/metadc62281/