386-679-6389 ●
OBJECTIVE To use my design and problem solving skills in the areas of FEA, CAE, Structural Engineering, Stress Engineering and Mechanical Design.
EDUCATION Master of Science in Aerospace Engineering, CGPA 3.27/4.0 May 2015
EMBRY-RIDDLE AERONAUTICAL UNIVERSITY Daytona Beach, FL
Bachelor of Science in Aeronautical Engineering, CGPA 3.62/4.0 June 2011
ANNA UNIVERSITY-CHENNAI Tamil Nadu, India
COMPUTER Design Software: Autocad, Pro-E, Catia v.5.
SKILLS Analysis Software: Abaqus, Ansys 14 and Ansys 14 Workbench
Pre/Post Processor: Femap
Solver: Nastran, Matlab
Application Software: MS word, MS excel, MS powerpoint.
PROFESSIONAL -Completed in-plant training on “Safe transportation of Hazardous Goods” at “Ashok Leyland” in Chennai- India.
ACTIVITIES -Completed a six month certification course on Catia v.5 (Part Design, Assembly Design, Drafting, Sheet Metal
Design and Generative Shape Design) and Ansys 14(Mechanical APDL and Workbench) at CADD center.
PROJECT Analysis of BOEING 767 Winglets – Tested and analyzed different mode frequencies generated for different
EXPERIENCE ‘Winglet Cant Angles’ using FEMAP/Nastran Software. Utilized Boeing 767 characteristics and data.
Determination of a Multi Body Dynamics system(MBD) – Calculated the natural frequencies
Of a 4 Degree of Freedom Semi- definite system carrying disks. Calculated the equations of motion of the system.
Used MATLAB program to compute the natural frequencies and corresponding mode shapes
Thermal Stress Analysis of a Bi-Metallic strip – Performed a thermal analysis on a Bi-Metallic strip of given dimension. Applied Loads to calculate the stress and applied temperature on both the surface of the strip to calculate the temperature distribution. Used FEMAP/ NEiNastran software to validate the result.
Structural Dynamic Analysis of Nose Landing Gear(FEA) – Performed structural analysis of a landing gear using CATIA and ANSYS Mechanical APDL 14.5. Obtained an analytical solution using MATLAB and hand calculations. Compared the results obtained from commercial software (CATIA/ ANSYS) with the hand calculations to validate the results and to check the airworthiness of the landing gear.
Morphing wing using Macro Fiber Composite Actuators - Designed a morphing wing model with suitable dimensions using CATIA V-5 and analyzed its effects when the model is subjected to load or force using ANSYS.
...
Login or Register to view the full resume.
