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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 38

An illustration from 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, leaf 38

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