Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration

Author:	Rumsey, Charles B.
Year:	1955
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L55G28A
Series:	NACA research memorandum ;
Report Number:	L55G28A
Subjects:	Heat--Transmission
	Charts, diagrams, etc
	Mathematics
	Temperature measurements
	Cylinders--Aerodynamics
	Aerodynamic heating
	Cone--Aerodynamics
	Aerodynamics, Supersonic
	Body of revolution
Link:	https://hdl.handle.net/2027/mdp.39015086465922