Preliminary results from a free-flight investigation of boundary-layer transition and heat transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x 10⁶

Author:	Hall, J. R.
Additional Authors:	Piland, Robert O., Speegle, Katherine C.
Year:	1957
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/L57D18c
Series:	NACA research memorandum ;
Report Number:	L57D18c
Subjects:	Heat--Transmission
	Boundary layer
	Thermal boundary layer
Link:	https://hdl.handle.net/2027/mdp.39015086507186