Title: Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2.05, 2.54, and 2.04
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003809150&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003809150&ix=nu&I=0&V=D&pm=1</a>
Subjects: Aerodynamics--Research, Drag (Aerodynamics.