Wind-tunnel investigation of effects of tail length on the longitudinal and lateral stability characteristics of a single-propeller airplane model
Description: Report presenting an investigation of a powered model of a single-propeller low-wing airplane with three values of tail length and three horizontal tails to determine the effects of tail length and tail volume on the longitudinal and lateral stability.
Date: December 1948
Creator: Johnson, Harold S.
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Partner: UNT Libraries Government Documents Department