
Worked on the sofia-ys/Aircraft-Design repository, delivering core simulation and analysis features for aircraft structural and aerodynamic modeling. Over three months, developed robust torque and thrust modeling with angle-of-attack dependencies, implemented class iteration support, and expanded torque constants for broader design coverage. Enhanced structural analysis by introducing column buckling safety margin calculations and visualization, including revised stress formulas and end-condition modeling. Integrated Overleaf versioning for documentation workflows and improved data management using Python and CSV. The work emphasized simulation fidelity, maintainable code structure, and clear data visualization, reducing engineering risk and supporting faster, more accurate design decision-making in aerospace contexts.
Month 2025-01 – sofia-ys/Aircraft-Design: Delivered core feature enhancements to structural analysis and expanded design data, strengthening safety assessment and design decision support. Key enhancements include: (1) Column buckling safety margin analysis and visualization improvements with a dedicated analysis script to compute and plot safety margins along wingspan, revised stress calculation formula, and updated end-condition modeling (K/L parameters) and visualization highlighting the minimum margin; (2) Torque constants data expansion adding -6 and 10 degrees constants to broaden torque analysis options in the design workflow. These changes improve risk assessment, reduce iteration time, and broaden the data foundation for torque-driven design.
Month 2025-01 – sofia-ys/Aircraft-Design: Delivered core feature enhancements to structural analysis and expanded design data, strengthening safety assessment and design decision support. Key enhancements include: (1) Column buckling safety margin analysis and visualization improvements with a dedicated analysis script to compute and plot safety margins along wingspan, revised stress calculation formula, and updated end-condition modeling (K/L parameters) and visualization highlighting the minimum margin; (2) Torque constants data expansion adding -6 and 10 degrees constants to broaden torque analysis options in the design workflow. These changes improve risk assessment, reduce iteration time, and broaden the data foundation for torque-driven design.
Month: 2024-12 - consolidated design-analysis work for sofia-ys/Aircraft-Design, delivering concrete torque-analysis capabilities and a solid groundwork for buckling analysis. Focused on delivering business-value by increasing design accuracy, reducing manual analysis time, and establishing a maintainable codebase for future enhancements.
Month: 2024-12 - consolidated design-analysis work for sofia-ys/Aircraft-Design, delivering concrete torque-analysis capabilities and a solid groundwork for buckling analysis. Focused on delivering business-value by increasing design accuracy, reducing manual analysis time, and establishing a maintainable codebase for future enhancements.
November 2024 monthly wrap-up for sofia-ys/Aircraft-Design: Focused on delivering core modeling capabilities, robustness improvements, and documentation support to accelerate simulation work and reduce engineering risk. Delivered features include class handling and iteration support across contexts (class-2 scenarios), Overleaf version integration for documentation workflows, robust drag behavior fallback to handle failure scenarios, bending file introduction for enhanced modeling fidelity, AoA calculations with support for multiple angles, and thrust modeling improvements including AoA-dependent thrust. Torque module refinements (lift handling and API cleanups) and miscellaneous placeholders scaffolding were also progressed. Major bug fixes include correcting torque unit conversions from Nm to kNm and adding missing torque usage examples. Overall, these changes improve simulation fidelity, reliability, onboarding, and integration with external documentation workflows.
November 2024 monthly wrap-up for sofia-ys/Aircraft-Design: Focused on delivering core modeling capabilities, robustness improvements, and documentation support to accelerate simulation work and reduce engineering risk. Delivered features include class handling and iteration support across contexts (class-2 scenarios), Overleaf version integration for documentation workflows, robust drag behavior fallback to handle failure scenarios, bending file introduction for enhanced modeling fidelity, AoA calculations with support for multiple angles, and thrust modeling improvements including AoA-dependent thrust. Torque module refinements (lift handling and API cleanups) and miscellaneous placeholders scaffolding were also progressed. Major bug fixes include correcting torque unit conversions from Nm to kNm and adding missing torque usage examples. Overall, these changes improve simulation fidelity, reliability, onboarding, and integration with external documentation workflows.

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