sofia-ys/Aircraft-Design
Nov 2024 – Jan 2025
3 Months active
Languages Used
PythonXML
Technical Skills
AerodynamicsAerospace EngineeringData ParsingData VisualizationFile HandlingFlight Dynamics
Jambuska
PROFILE
Jambuska
Bence Gecseg developed advanced aerodynamic and structural analysis tooling for the sofia-ys/Aircraft-Design repository, focusing on Python-based simulation and data visualization. Over three months, he delivered modules for Mach-aware lift distribution, angle of attack solvers, and torque-induced shear flow analysis, integrating these with existing wing-structure components. His work included enhancements to shear buckling calculations, average shear stress analysis, and critical skin buckling assessment, leveraging NumPy and numerical methods to improve simulation accuracy. By refactoring modules and addressing key bugs, Bence improved maintainability and reliability, enabling faster design validation and supporting data-driven decisions in aerospace engineering workflows.
Overall Statistics
Feature vs Bugs
82%Features
Repository Contributions
32Total
Bugs
2
Commits
32
Features
9
Lines of code
1,563
Activity Months3
Your Network
9 peopleWork History
January 2025
6 Commits • 3 Features
Jan 1, 2025January 2025 – Aircraft-Design (sofia-ys/Aircraft-Design) monthly summary: Delivered three core tooling features to strengthen wing structural analysis, improved modeling capabilities for shear and buckling, and reinforced integration with existing wing-structure modules. No major bugs reported; minor formatting and integration improvements completed to ensure reliability and repeatability. These changes enable faster design validation, reduce risk of structural errors, and support data-driven design decisions. Key outcomes include: - new avg shear stress tooling (avg_shear.py and avg_shear2.py) integrated with wing-structure modules; - torque-induced shear flow analysis module (shear_flow.py) with multi-configuration support; - enhanced shear/stress and buckling analysis with Wing_Box_Detailed calculations and plotting across components. Commits demonstrating this work include: 5fff01d99c001866925ca613825f5189cf4d1f42; 096a12a203a65b5fd8d345a04f44cab5537069d1; 7c22d7af11e952426e259274a21f8a6940323ab6; 6b424f32198a0c0a3900bbd3b64a3853c35dad71; c4c8a0a8fc9bca04aaea9a5f35e42e8da549a6d0; ae3eebaf8738b0f4a4c847435fae587b2b631110.
6 Commits • 3 Features
Jan 1, 2025January 2025 – Aircraft-Design (sofia-ys/Aircraft-Design) monthly summary: Delivered three core tooling features to strengthen wing structural analysis, improved modeling capabilities for shear and buckling, and reinforced integration with existing wing-structure modules. No major bugs reported; minor formatting and integration improvements completed to ensure reliability and repeatability. These changes enable faster design validation, reduce risk of structural errors, and support data-driven design decisions. Key outcomes include: - new avg shear stress tooling (avg_shear.py and avg_shear2.py) integrated with wing-structure modules; - torque-induced shear flow analysis module (shear_flow.py) with multi-configuration support; - enhanced shear/stress and buckling analysis with Wing_Box_Detailed calculations and plotting across components. Commits demonstrating this work include: 5fff01d99c001866925ca613825f5189cf4d1f42; 096a12a203a65b5fd8d345a04f44cab5537069d1; 7c22d7af11e952426e259274a21f8a6940323ab6; 6b424f32198a0c0a3900bbd3b64a3853c35dad71; c4c8a0a8fc9bca04aaea9a5f35e42e8da549a6d0; ae3eebaf8738b0f4a4c847435fae587b2b631110.
January 2025
December 2024
16 Commits • 3 Features
Dec 1, 2024December 2024 monthly performance summary for sofia-ys/Aircraft-Design focusing on delivering core aerodynamic tooling improvements and enhanced structural analysis capabilities.
December 2024
16 Commits • 3 Features
Dec 1, 2024December 2024 monthly performance summary for sofia-ys/Aircraft-Design focusing on delivering core aerodynamic tooling improvements and enhanced structural analysis capabilities.
November 2024
10 Commits • 3 Features
Nov 1, 2024November 2024 (2024-11) focused on delivering data-driven aerodynamics and robust structural loading capabilities for Aircraft-Design, while improving maintainability and addressing a critical load calculation bug. Key outcomes include: 1) Python-based Aerodynamics Data Import and Mach-Number Lift Distribution with Mach-aware lift updates; 2) Wing Structural Loads and MTOM-based Calculations, including shear, bending moment distributions, MTOM-based loads, and landing gear load refinements; 3) Wing Structure Module Refactor and Cleanup to support future development; 4) Bug fix for Fuel Fraction Handling in Distributed Load, correcting absolute value usage. All work is traceable to commit references in sofia-ys/Aircraft-Design.
10 Commits • 3 Features
Nov 1, 2024November 2024 (2024-11) focused on delivering data-driven aerodynamics and robust structural loading capabilities for Aircraft-Design, while improving maintainability and addressing a critical load calculation bug. Key outcomes include: 1) Python-based Aerodynamics Data Import and Mach-Number Lift Distribution with Mach-aware lift updates; 2) Wing Structural Loads and MTOM-based Calculations, including shear, bending moment distributions, MTOM-based loads, and landing gear load refinements; 3) Wing Structure Module Refactor and Cleanup to support future development; 4) Bug fix for Fuel Fraction Handling in Distributed Load, correcting absolute value usage. All work is traceable to commit references in sofia-ys/Aircraft-Design.
November 2024
Activity
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Quality Metrics
Correctness77.8%
Maintainability80.0%
Architecture72.4%
Performance67.6%
AI Usage20.0%
Skills & Technologies
Programming Languages
PythonXML
Technical Skills
AerodynamicsAerodynamics SimulationAerospace EngineeringBytecode analysisCFDCode CommentingComputational Fluid DynamicsData AnalysisData ParsingData VisualizationFile HandlingFinite Element AnalysisFlight DynamicsFlight MechanicsInterpolation
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