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What is Wing and Fuselage Effects on Tail Roll about?

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