William T. O'Bryant · 2 obras en el catálogoObrasAn experimental investigation of hypersonic flow over blunt nosed cones at a Mach number of 5.8.EExperimental Investigation of Hypersonic Flow over Blunt NosExperimental Investigation of Hypersonic Flow over Blunt Nosed Cones at a Mach Number Of 5. 8
EExperimental Investigation of Hypersonic Flow over Blunt NosExperimental Investigation of Hypersonic Flow over Blunt Nosed Cones at a Mach Number Of 5. 8