Resume Templates: Research Assistant

Aja Kam
123 Madeup Ave,Null Street, CA | Cell: 123-456-7890 | Email: thisisntreal@fake.com

SUMMARY
Innovative Mechanical Engineer who improves development plan execution by consistently creating new formulations and techniques. A team-oriented professional who works effectively with all levels of employees in cross-functional teams to achieve organizational goals. Fluent in English and Hindi.

TECHNICAL COMPETENCIES
ANSYS CFX; ANSYS Fluent; ANSYS Turbogrid; Pointwise; Bladegen; ICEM; NASTRAN; MATLAB; Simulink, CATIA V5; Autodesk AUTOCAD; UniGraphics; ABAQUS; Mechanical APDL; Microsoft Office TURBOMACHINERY APPLICATION ENGINEERING INTERN Softinway, Inc. Daytona Beach Provided key contributions within Micro Gas Turbines and the overall power plant structure. Developed test cases and validation studies for aero-thermodynamic issues. Analyzed problems with power plants and studied methods for optimization. Acquired working knowledge of various power plants, including air-breathing gas, steam, and nuclear powered turbines. Engaged in cycle, mean-line, streamline and 3D-Blade designs of axial turbines, radial compressors, axial compressors and centrifugal compressors. Conducted stress analyses and CFS on turbo-machinery components. RESEARCH ASSISTANT, Gas Turbine Laboratory Embry-Riddle Aeronautical University Daytona Beach, FL Conducted compressor design and surge mitigation utilizing CFD while writing a thesis on controlling surge by designing a multi-spool, high-pressure compressor. Used counter-rotation, ANSYS Bladegen and mean-line analysis within the compressor design. Created a detailed analysis to compare numerical results with CFD results, including stall conditions forced on the compressor and staff recovery analysis, varying the RPM. Collaborated on a proprietary integrated jet engine with an electric compressor system without shaft and an electric generator. Designed compressor stages to work independently with sequential counter-rotation, and optimized RPM within any flight condition. Modified the engine control system utilizing FADEC. Contributed to the development of a super-conduction cooling system for efficient operation with lower power requirements. Collaborated with a Boeing duct tool design, working with a five-member team to create a proprietary duct tool system aiding in the design of ducts for various parts within the jet engine, including nacelles and bleeds.

EXPERIENCE
08/2014 to 10/2014

08/2012 to 07/2014

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