Building engineering tools that serve 190+ engineers on Turkey's 5th-generation fighter aircraft program
I combine deep aerospace structural analysis expertise with software engineering to create tools that automate FEA workflows, visualize complex results, and accelerate aircraft development.
I am a Senior Structural Analysis Engineer at Turkish Aerospace, working on the TF-X (KAAN) 5th-generation fighter aircraft program. Over the past 5+ years, I have performed static stress analysis, sizing, and design optimization of composite and metallic center fuselage structures across three aircraft generations (P0, Block 0, Block 10).
Recognized as the top-performing engineer among 130+ analysts in two consecutive years, I combine deep structural mechanics knowledge with a passion for software development. I have built 12 production-grade tools that automate FEA workflows, from interactive 3D visualization to automated strength analysis, serving the entire department of 190+ engineers.
My tools address real engineering challenges: mapping properties between mesh configurations, calculating fastener stiffness, filtering 100GB+ datasets, and generating interactive stress reports. Each tool is built with professional GUIs, parallel processing, and robust file handling for Nastran models.
A unique blend of aerospace structural analysis and software engineering.
Production-grade tools automating FEA workflows for the aerospace industry. Click any card for details.
Interactive 3D mesh visualization generating S2D HTML reports. The standard data transfer method between 130+ analysis and 60+ design engineers.
Generalized metaheuristic optimization framework using Excel, executables, or ML models as evaluators. Supports single and multi-objective optimization with 10 algorithms.
Multi-process automation orchestrating HyperMesh and Excel for end-to-end bolted joint analysis of composite and metallic aircraft structures.
Automated von Mises strength analysis with intelligent element classification by connection type and vectorized thickness optimization.
Extracts buckling mode data from Nastran results with structural connectivity analysis, coplanar property detection, and T-connection awareness.
Calculates CBUSH fastener stiffness using the Huth formula with CLT composite support, multi-plate analysis, and Airbus method dual-CBUSH generation.
Intelligent property transfer between FE meshes using proximity analysis, surface normal alignment, and ray casting with 5-level confidence assessment.
Automatically generates RBE2/RBE3 rigid body elements with spatial algorithms, exclusive assignment modes, and colinearity detection.
High-performance BDF/CSV filtering with streaming architecture for 100GB+ files, entry-aware processing, and complex Boolean expressions.
Maps thermal loads between non-conforming FE meshes using KNN interpolation with inverse distance weighting for coupled thermal-structural analysis.
Interpolates prescribed displacement loads between meshes, preserving load case structure and DOF definitions for boundary condition transfer.
Comprehensive HyperMesh plugin with 75+ procedures for FEM model preparation, fastener modeling, quality checks, and analysis setup.
Building aircraft structures and the tools to analyze them.
Turkish Aerospace — TF-X (KAAN) 5th Generation Fighter Aircraft
Turkish Aerospace — Satellite Structural Testing
Mechanical Engineering
Thesis: Graph Neural Networks as Surrogate Models for Structural Analysis: A Study on Buckling Behavior
Mechanical Engineering
CGPA: 3.68 / 4.00 — Ranked 1st in class
Whether it's about aerospace engineering, tool development, or potential collaboration.