- Ankara, Turkiye
- in/mklbozdogan
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panel-method-solver
panel-method-solver PublicMATLAB implementation of the source panel method for two-dimensional airfoil analysis.
MATLAB 1
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glider-range-optimization
glider-range-optimization PublicMATLAB-based glider design and trajectory simulation for maximum range under fixed design constraints.
MATLAB 1
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afterburning-turbojet-performance-analysis
afterburning-turbojet-performance-analysis PublicMATLAB-based afterburning turbojet engine performance analysis using atmospheric data and cycle calculations.
MATLAB 1
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airfoil-critical-mach-optimization
airfoil-critical-mach-optimization PublicMATLAB-based CST airfoil optimization for maximizing critical Mach number using panel method analysis.
MATLAB 1
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