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Resume Updated: 10 Jan 2010
Vadivel kumaran Sivashanmugam
Tel: 0015145780533 Fax:
1433, Rue Towers, Apt 209
Montreal, Quebec

Looking for a challenging position as an aeronautical/mechanical engineer in an environment where I can apply my expertise in CFD, FEA and optimization to develop new designs, and also provides the opportunity for my further professional growth.
Salary Requirements
$55,000 to $65,000 per annum
Employment History
Research Assistant Jan 2008- present
Concordia University
Montreal, Canada
Thesis Title: Aero - structural shape optimization of turbomachinery Blades Evaluated aerodynamic performance of turbine blades using ANSYS CFX Analyzed turbine blade stress and vibration using ANSYS Workbench Simulation. Implemented multiple artificial neural network modules in C++ for multi disciplinary optimization (MDO) Performed aero - structural shape optimization of turbomachinery blades using artificial neural networks (ANN) and genetic algorithms (GA) Kept abreast with technical advancements in computational tools (CFD, FEA and optimization techniques) and turbomachinery design
Intern & Finite element engineer Dec 2008 - present
Ohive Inc.
Performed static, dynamic and vibration analysis for mechanical components (Heavy Machinery) Undergoing MSc SimXpert certification training from MSc Software corporation Resolved issues within strict time limits
Aerospace engineer Oct 2003 - July 2007
CEMILAC, Defence Research and Development Org. (DRDO), Ministry of Defence, Indi
Hyderabad, India
Verified structural analysis results for airframe and other subsystems and specified qualification test schedules Member of store separation analysis (CFD) team for air launched missiles Lead the team of four and successfully evaluated the design and integration process of Counter Measure Dispensing System (CMDS) (to deceive IR seeking & Radar guided missiles) for Advanced Light Helicopter and Jaguar A/c Coordinated technical meetings with various industry, research and certification organizations
Master of Applied Sciences (M.A.Sc), Mechanical Engineering (Aerospace), Concordia University, Montreal, Quebec, Canada
Thesis Title: Aero - Structural shape Optimization of Turbomachinery Blades
Courses: Gas Turbine Design, Stress analysis, Aerodynamics, Aircraft Structures etc
Year: Jan 2008 Feb 2010 (Expected)

Bachelor of Technology, Aeronautical Engineering, Madras Institute of Technology, Anna University, India
Courses: Aircraft & Missile propulsion, Gas Dynamics, CFD, FEM, Aircraft performance & Stability etc.
Year: 1999 2003
Description Proficiency Experience
C programming Expert >5 Years
C++ programming Expert >5 Years
CFD analysis Advanced 2-3 Years
FEA analysis Advanced 2-3 Years
Turbomachinery design Intermediate 1-2 Years
Additional Skill Info
Engineering Skills Optimization Techniques, Solid Modeling Software Skills C, C++, MATLAB, ANSYS WORKBENCH (ICEMCFD, CFX, FLUENT & SIMULATION), NASTRAN, PATRAN, GAMBIT, ALGOR & CATIA V5R18
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