Mayank Parmar

Damage tolerance analysis, Fatigue analysis

Software: Hyperwork, Msc. Nastran, Msc. Patran, VBA, Awk, Shell, Pcl, Mathcad - Stress analysis of the parts of the fuselage structure - Comparison of the results achieved by different design fastening conditions - Buckling Analysis - Development of buckling interaction formula for various supporting and loading conditions

Simulation of Non-linear Degradation of Hybrid Material Joints in Civil Aircraft Structure. Software: Hyperwork, Msc. Nastran, Python, Pro-E - Double Cantilever Beam (DCB) and End notched flexure (ENF) toughness test performed - FEA analysis for the Mode-I (DCB) and Mode-II (ENF) failure prediction using fracture mechanics (VCCT) approach - Implementation of Virtual crack closure technique (VCCT) for debonding in global fuselage structure

Software: Pro-E, Ansys(Workbench) - Worked for the designing and development of the Bearing Assembly machine. - CAD Modeling using Pro-E (Creo) - FEA Modeling using Ansys workbench - Stress analysis of 3D bearing model with hub

Analysis of Bearing assembly machine and elimination of the undesirable Components Software: Pro – E and Ansys (workbench) - Optimization of the assembly Process and definition of the new design - Redesigned the assembly machine using Pro-E

Finite element methods, Computational fluid dynamics, Thermodynamics of materials, Analysis of structure

Machine design, Thermodynamics, Kinematics of machine, Theory of machine