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Airplane stability for flight with constant angular velocity around the longitudinal axis(Effects of longitudinal acceleration and Magnus forces and moments on stability of aircraft with constant velocity around longitudinal axis)
A problem of optimal control with constraints on the coordinates of the center of mass(Ob odnoi zadache optimal'nogo upravleniia pri ogranicheniiakh na koordinaty tsentra mass)
Performance evaluation method for dissimilar aircraft designs(using the square of the wing span for nondimensional comparisons of aerodynamic characteristics)