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
This is a 1950 NACA technical report, issued by the National Advisory Committee for Aeronautics, presenting force measurements from wind-tunnel tests of the RM-10 missile at Mach numbers 1.49 to 1.98 for aerodynamics engineers. Its pictures are plain engineering graphs of pitching-moment, drag and centre-of-pressure curves against angle of attack, with data points and theory lines that a designer could read as a clear, restrained chart style.
