Determination of the longitudinal moment coefficient of an aircraft with wing tips

Authors

  • Hanna Borysiuk National Aviation University
  • Oleksandr Yakushenko National Aviation University
  • Volodymyr Miltsov National Aviation University
  • Maksym Borysiuk National Aviation University

Keywords:

longitudinal moment wing, mathematical model, AT winglet, centering

Abstract

Using the expressions for the coefficient of the longitudinal moment for an aircraft with a wing without wingtips, the longitudinal moment coefficient for the aircraft with a wing with aerodynamic ends was recorded, and its derivatives were calculated.

Additional Files

Published

2025-03-28

Issue

2024: XI Всесвітній конгрес “Авіація в XXI столітті” – “Безпека в авіації та космічні технології”

Section

Engines and power plants