A Summary of the Longitudinal and Lateral Stability and Control Characteristics Obtained from Rocket-model Tests of a Swept-wing Fighter-type Airplane at Mach Numbers from 0.5 to 1.9

NASA Technical Reports Server (NTRS) · 1957 · 10 pictures

NASA Technical Reports Server (NTRS)

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