Heat transfer and pressure measurement on a 5-inch hemispherical concave nose at a Mach number of 2.0

Author:	Markley, J. Thomas.
Year:	1958
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/L58C14a
Series:	NACA RM ;
Report Number:	L58C14a
Subjects:	Heat--Transmission
	Noses (Aircraft)
	Skin friction (Aerodynamics)
Link:	https://hdl.handle.net/2027/mdp.39015086466342