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Wing and Fuselage Effects on Tail Roll by tasteless.tuna.hsbp is a document available to read on EtoBox.
This document presents an investigation into the influence of wing and fuselage on the vertical-tail contribution to the low-speed rolling derivatives of midwing airplane models with 45° sweptback surfaces. The findings indicate that the vertical-tail contribution can be accurately calculated when corrections for fuselage and wing effects are applied, although the fuselage
- Author
- tasteless.tuna.hsbp
- Language
- EN