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, by Charles B. Rumsey et al.

Title:	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.
Author:	Langley Aeronautical Laboratory
Author:	United States. National Adviosry Committee for Aeronautics
Author:	United States. National Advisory Committee for Aeronautics
Note:	National Advisory Committee for Aeronautics, 1955

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Subject:	Aerodynamic heating
Subject:	Aerodynamics, Supersonic
Subject:	Body of revolution
Subject:	Charts, diagrams, etc.
Subject:	Cone -- Aerodynamics
Subject:	Cylinders -- Aerodynamics
Subject:	Heat -- Transmission
Subject:	Mathematics
Subject:	Temperature measurements
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