Detailed pressure distribution on a blunted 60-deg half-angle cone at Mach numbers of 6.08 and 9.46
Pressure distribution of spherically-blunted 60 deg half-angle cone in hypersonic flow
Kurtz, D. W.↗
Engineering topics
Kurtz, D. W.
Publications and source records attributed to Kurtz, D. W..
Forebody effects on drogue drag in supersonic flow.
Forebody shape effects on drogue drag tested for various forebody-drogue configurations in supersonic flow
Dayman, B., Jr.↗