Heat-Transfer and Pressure Measurements from a Flight Test of a 1/18-Scale Model of the Titan Intercontinental Ballistic Missile Up to a Mach Number of 3.95 and Reynolds Number Per Foot of 23 by 10 to the 6th Power

Author:	Graham, John B., Jr.
Additional Authors:	Chauvin, Leo T.
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-SL57L16A
Link:	https://digital.library.unt.edu/ark:/67531/metadc53269/