Imran Muhammad

“A350-900 wing upper cover composites interfaces analysis’’ • Stress check and static analysis of the composite wing upper cover leading and trailing edge interfaces. • Model preparation from detailed FE model and Filled Hole Analysis in ISAMI. • Mitigations for critical reserve factors. • Assessment of manufacturing non-conformities, oversize concessions. Software used: • Nastran/Patran, ISAMI, MS-office macro, Unix.

Sizing and Optimization of A350 XWB 900 MSN-17 Section 16-18’’ • Optimization analysis of cut-outs in lower shell rear part of fuselage. • Linear static and buckling analysis of detailed FE model. • Analytical calculations using HSB methods. • Calculation of buckling and edge impact reserve factors to ensure strength and stability of composite structure. Software used: Hypermesh, OptiStruct, Radioss, Nastran/Patran.

“Mechanical design and technical support’’ • Designing and thermal analysis of electrical PCBs housings. • Generation of CNC codes for milling of housings. • Designing and static analysis of fixtures for test support. Software used: Pro-E, Ansys Workbench 12.

• To assist in manufacturing planning and control in machine shop. • Inspection of incoming materials. • Final dimensional inspection.

Linear & non-linear FEM, Numerical methods, materials modeling, Composite materials.

Engineering drawing, Machine design, Mechanics of materials