Murat Günel

HURKUS Project Front-Center Fuselage System Installation Stress Responsible Detailed Stress Analysis of Metallic and Composite Parts by Using Hand Calculations (Bruhn,Niu,ESDU,etc.),Developed Analysis Tools and FEM (MSC.Patran/Nastran/Mentat/Marc).

Progressive Failure Analysis, Linear/Non-Linear Mechanics of Composite Materials, Finite Element Applications for Advanced Engineering Problems Final Year Project: Progressive Failure Analysis of Laminated Composite Materials by using Patran Command Language (PCL)

Stress and Design of Aircraft Structures. Final Year Subjects: Preliminary UAV Design, Mechanics of Composites. Final Year Project: Parametric Design Tool Development for A400M Wing Spar in MSC.Patran by using PCL (TAI cooperative)