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 (1957)
NASA Technical Reports Server (NTRS) · leaf 65
<Js 4=" NACA RM L56K19 of tail deflection. Change in lift coefficient per degree Figure 51*-
NASA Technical Reports Server (NTRS)
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