Time-vector Determined Lateral Derivatives of a Swept-wing Fighter-type Airplane with Three Different Vertical Tails at Mach Numbers Between 0.70 and 1.48
This is a NACA research memorandum from 1956, issued by the United States National Advisory Committee for Aeronautics, reporting wind-tunnel measurements of lateral stability derivatives for a swept-wing fighter airplane with three vertical tail configurations across Mach 0.70 to 1.48, written for aeronautical engineers. The pictures are dense technical plots: multi-panel graphs of coefficients against Mach number with dashed and solid curves, scatter points with leader-line labels, and vector diagrams with tabulated values, all in a restrained black-and-white grid style a designer might borrow for diagrammatic structure.
