Measurements of the Mach Number and Pressure on the Afterbody of a Blunt-Nosed Model in Free Flight at Mach Numbers from 6.5 to 14
1960
16 pages
Report
No indication
English
Aerodynamics , Afterbody , Blunt body , Hypersonic speed , Mach number , Pressure measurement , Aerodynamic , Blunt , Body , Drag , Flight , Flow , Free , Free flight , Heating , Hypersonic , Local , Measurement , Model , Nose , Pressure , Shock , Speed , Stability , Static , Stream , Test , Tunnel , Wave , Wind