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Time-vector Determined Lateral Derivatives of a Swept-wing Fighter-type Airplane with Three Different Vertical Tails at Mach Numbers Between 0.70 and 1.48

C. H. Wolowicz

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Key concepts: Airplane, Wing, Mach number, Aerospace engineering, Physics, Mathematics, Structural engineering, Aeronautics

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Time-vector Determined Lateral Derivatives of a Swept-wing Fighter-type Airplane with Three Different Vertical Tails at Mach Numbers Between 0.70 and 1.48 — Research Paper | ScholarLens