Influence of Wing and Fuselage on the Vertical-Tail Contribution to the Low-Speed Rolling Derivatives of Midwing Airplane Models with 45 Degree Sweptback Surfaces
Description: Note presenting an investigation to determine the influence of the wing and fuselage on the vertical-tail contribution to the low-speed rolling derivatives of midwing airplane models with 45 degree sweptback surfaces. Results regarding the data presentation, characteristics of some basic configurations, interference effects, and tail contributions are provided.
Date: December 1951
Creator: Wolhart, Walter D.
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