1. Configurations that had zero-yaw drag coefficients less than 1.5 displayed the tendency to have multiple non-zero trim points and are therefore classified as a Type-4 oscillation. The body alone drag coefficient was 1.0 at zero-yaw angle. This indicates, as one would expect, that there minimum threshold required to consistently
2. Dynamics of Ribbon Stabilized M42 Grenade0022, U.S. Aviation and Missile Command Technical Report T-79-84, Redstone Arsenal,September 1979. (2) Dahlke,C-W. "Aerodynamic and