
Worked on the PURPL-Purdue/Turbopump repository, delivering features for thrust chamber and nozzle design automation. Developed Python scripts leveraging YAML configuration to drive thrust chamber calculations, streamline data export, and enhance plotting for engineering analysis. Improved DXF file handling and export paths, ensuring accurate and versioned geometry outputs for nozzle contours. Expanded thermodynamics modules to support performance plots under varying conditions, including oxidizer-to-fuel ratio analysis. Refactored data workflows to align with evolving directory structures, maintaining export reliability and integration compatibility. Applied skills in Python, CAD integration, and scientific computing to support rapid design iteration and data-driven decision-making in aerospace engineering contexts.
February 2026 (2026-02) performance summary for PURPL-Purdue/Turbopump. Delivered enhancements to thrust analysis via oxidizer-to-fuel (O/F) ratio range testing, expanding bounds and enabling computation of thrust across varying O/F ratios. Also completed a nozzle contour data export path refactor to align with the new directory structure, preserving export functionality and data integrity. Focused on expanding test coverage, improving data workflows, and ensuring export compatibility to support design decisions and downstream analytics.
February 2026 (2026-02) performance summary for PURPL-Purdue/Turbopump. Delivered enhancements to thrust analysis via oxidizer-to-fuel (O/F) ratio range testing, expanding bounds and enabling computation of thrust across varying O/F ratios. Also completed a nozzle contour data export path refactor to align with the new directory structure, preserving export functionality and data integrity. Focused on expanding test coverage, improving data workflows, and ensuring export compatibility to support design decisions and downstream analytics.
Monthly summary for 2025-12: Delivered core features for nozzle visualization, data management, and thermodynamics-driven performance plots in PURPL-Purdue/Turbopump. Achievements span visualization enhancements, DXF data handling improvements, and expanded thermodynamics calculations, translating into clearer design insights, more reliable data exports, and faster decision-making in nozzle/pump design under varied conditions.
Monthly summary for 2025-12: Delivered core features for nozzle visualization, data management, and thermodynamics-driven performance plots in PURPL-Purdue/Turbopump. Achievements span visualization enhancements, DXF data handling improvements, and expanded thermodynamics calculations, translating into clearer design insights, more reliable data exports, and faster decision-making in nozzle/pump design under varied conditions.
November 2025 monthly summary for PURPL-Purdue/Turbopump: Delivered config-driven TCA calculations with YAML-based configuration, reorganized TCA directory, and updated thrust chamber parameters; upgraded DXF export and nozzle contour data with unit conversions and improved export paths; enhanced plotting and visualization with YAML-driven, inches-based plots and annotated contour visuals. These changes improve data accuracy, reproducibility, and decision speed for design iterations.
November 2025 monthly summary for PURPL-Purdue/Turbopump: Delivered config-driven TCA calculations with YAML-based configuration, reorganized TCA directory, and updated thrust chamber parameters; upgraded DXF export and nozzle contour data with unit conversions and improved export paths; enhanced plotting and visualization with YAML-driven, inches-based plots and annotated contour visuals. These changes improve data accuracy, reproducibility, and decision speed for design iterations.

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