Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings

Goodman, Alex Fisher, Lewis R
naca-report-968
1950


A low-scale wind-tunnel investigation was conducted in rolling flow to determine the effects of aspect ratio and sweep (when varied independently) on the rolling stability derivatives for a series of untapered wings. The rolling-flow equipment of the Langley stability tunnel was used for the tests. The data of the investigation have been used to develop a method of accounting for the effects of the drag on the yawing moment due to rolling throughout the lift range.

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