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- Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration have a 60©� delta wing and a high unwept horizontal tail
- Control hinge-movement and effectiveness characteristics of several interchangeable tip controls on a 60©� delta wing at Mach numbers of 1.41, 1.62, and 1.96
- Calculated effects of the lateral acceleration derivatives on the dynamic lateral stability of a delta-wing airplane