
Goga Myak developed and enhanced core simulation and analysis features for the sofia-ys/Aircraft-Design repository, focusing on structural and aerodynamic modeling. Over three months, Goga implemented torque and thrust modeling with angle-of-attack dependencies, introduced robust drag fallback mechanisms, and expanded buckling analysis capabilities, including safety margin visualization along the wingspan. Using Python and Matplotlib, Goga improved data-driven design workflows by refining stress calculations, updating end-condition modeling, and broadening torque constants for more comprehensive analysis. The work emphasized maintainable code, clear documentation, and integration with external tools, resulting in deeper simulation fidelity and more reliable engineering decision support for aircraft 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 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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