Title: Heat transfer and pressure measurement on a 5-inch hemispherical concave nose at a Mach number of 2.0
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003834297&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003834297&ix=nu&I=0&V=D&pm=1</a>
Subjects: Skin friction (Aerodynamics, Noses (Aircraft, Heat--Transmission.