Aerodynamic Characteristics of NACA RM-10 Missile in 8- by 6-foot Supersonic Wind Tunnel at Mach Numbers from 1.49 to 1.98 II : Presentation and Analysis of Force Measurements

NASA Technical Reports Server (NTRS) · 1950 · 4 pictures

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work) · More from this library