
Developed advanced heat exchanger sizing and thermal analysis features for the huciupaul/SHTARWaRS repository, supporting hydrogen storage and pressurized coolant configurations. Enhanced the constraint and performance analysis workflow for the Beechcraft 1900D by introducing modular scripting, a power-to-weight performance metric, and improved data visualization, including new design points such as TOGA. Finalized and stabilized the analysis pipeline to enable repeatable design studies and faster iteration cycles. The work leveraged Python for scientific computing, simulation, and data analysis, with a focus on aerodynamics, thermodynamics, and performance modeling to support robust aerospace engineering design and reproducible trade studies.
May 2025 performance summary for huciupaul/SHTARWaRS: Implemented heat exchanger sizing and thermal analysis enhancements with hydrogen storage and pressurized coolant support; enhanced constraint and performance analysis for Beechcraft 1900D with modular scripting, power-to-weight metric, improved plotting/visualization, and TOGA design points; finalization of constraint diagrams and stabilization of the analysis pipeline to enable repeatable design studies and faster iteration.
May 2025 performance summary for huciupaul/SHTARWaRS: Implemented heat exchanger sizing and thermal analysis enhancements with hydrogen storage and pressurized coolant support; enhanced constraint and performance analysis for Beechcraft 1900D with modular scripting, power-to-weight metric, improved plotting/visualization, and TOGA design points; finalization of constraint diagrams and stabilization of the analysis pipeline to enable repeatable design studies and faster iteration.

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