Effects of Surface Roughness and Extreme Cooling on Boundary-Layer Transition for 15 Degrees Cone-Cylinder in Free Flight at Mach Numbers to 7.6

Author:	Rabb, Leonard
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NASA-TM-79867, NACA-RM-E57K19
Link:	https://digital.library.unt.edu/ark:/67531/metadc53340/