
Adrien Esmiol developed and refined core simulation pipelines for the sofia-ys/Aircraft-Design repository, focusing on enhancing the accuracy and reliability of wing structural and aerodynamic analyses. He expanded the wing structural analysis workflow by implementing new shear and bending modules, integrating plotting capabilities, and refactoring data ordering for precise numerical integration. In parallel, Adrien improved aerodynamic data fidelity by updating main wing datasets and correcting XFLR5 simulation outputs, ensuring alignment with physical testing parameters. Leveraging Python for data processing, visualization, and modular architecture, his work established robust traceability between structural and aerodynamic models, supporting more informed and efficient design decisions.
Month: 2024-11 | Repository: sofia-ys/Aircraft-Design Overview: In November 2024, two key work streams were delivered to strengthen the reliability and fidelity of wing design simulations. The Wing Structural Analysis pipeline was expanded with new shear and bending modules, plotting capabilities, and refactoring to ensure correct data ordering and accurate integration. The Wing Aerodynamic Data refinement included updating data for the main wing and correcting XFLR5 outputs to reflect updated Beta, Phi, CL, Cd, Cl, Cm, XCP, YCP, ZCP and corresponding bending. These changes improve simulation fidelity, enable faster iteration, and provide stronger support for design decisions. Key outcomes include improved data integrity, end-to-end traceability between structural and aerodynamic analyses, and better alignment with physical testing expectations. Technologies/skills demonstrated: Python-based analysis pipelines, data processing and transformation, visualization/plotting, refactoring for modular architecture, and XFLR5 data integration.
Month: 2024-11 | Repository: sofia-ys/Aircraft-Design Overview: In November 2024, two key work streams were delivered to strengthen the reliability and fidelity of wing design simulations. The Wing Structural Analysis pipeline was expanded with new shear and bending modules, plotting capabilities, and refactoring to ensure correct data ordering and accurate integration. The Wing Aerodynamic Data refinement included updating data for the main wing and correcting XFLR5 outputs to reflect updated Beta, Phi, CL, Cd, Cl, Cm, XCP, YCP, ZCP and corresponding bending. These changes improve simulation fidelity, enable faster iteration, and provide stronger support for design decisions. Key outcomes include improved data integrity, end-to-end traceability between structural and aerodynamic analyses, and better alignment with physical testing expectations. Technologies/skills demonstrated: Python-based analysis pipelines, data processing and transformation, visualization/plotting, refactoring for modular architecture, and XFLR5 data integration.

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