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Geometry and dimensions of the horizontal tail finite element model. Key dimensions are annotated: wingspan (2988 mm), root chord (480 mm), tip chord (470 mm), root airfoil thickness (60 mm), and tip airfoil thickness (30 mm).

Journal: Scientific Reports

Article Title: Tolerance driven lightweight design and interface robustness of multi material aircraft horizontal tail structures

doi: 10.1038/s41598-026-35265-3

Figure Lengend Snippet: Geometry and dimensions of the horizontal tail finite element model. Key dimensions are annotated: wingspan (2988 mm), root chord (480 mm), tip chord (470 mm), root airfoil thickness (60 mm), and tip airfoil thickness (30 mm).

Article Snippet: A high-fidelity three-dimensional nonlinear finite element model was developed in ABAQUS/Standard (version 2022) to simulate the mechanical response of the multi-material horizontal tail under static aerodynamic loading.

Techniques: