Effect of an unswept wing on the contribution of unswept-tail configuration to the low-speed static and rolling-stability derivatives of a midwing airplane model

William Letko, Donald R. Riley
naca-tn-2175
Aug 1950


An investigation has been conducted in the Langley stability tunnel to determine the effect of an unswept wing on the contribution of unswept-tail configuration to the low-speed static- and rolling-stability derivatives of a midwing airplane model.

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