03.4 - Applied Aerodynamics

STUDY ON THE IMPACT OF TRIM CONDITION ON LATERAL AND DIRECTIONAL STABILITY FOR A TAILLESS AIRCRAFT

K. Kania, Warsaw University of Technology, Poland

This paper presents outcomes of the numerical study into the impact of the trim condition on the static stability for an unconventional, tailless aircraft. Both the quantitative and qualitative comparison is conducted based on the stability derivatives due to sideslip and visualizations generated using Ansys Fluent.

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DOI: 10.71945/icas2026_0330