G. M. Sakamoto

Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane

E. L. Friend, G. M. Sakamoto, 1978 .

Aerodynamic characteristics of a vane flow angularity sensor system capable of measuring flight path accelerations for the Mach number range from 0.40 to 2.54

G. M. Sakamoto, 1976 .