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NACA-ARR-L5F23: Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces
Abstract: INTRODUCTION
One of the many aerodynamic problems for which a theoretical solution by means of lifting-line theory might be expected to be inadequate is the case of a wing in steady roll. Robert T. Jones has obtained ...
One of the many aerodynamic problems for which a theoretical solution by means of lifting-line theory might be expected to be inadequate is the case of a wing in steady roll. Robert T. Jones has obtained ...