R a m a s a m y *
RS Vewen Ramasamy
269-***-**** 680 South Howard Street, Apt 302, Kalamazoo, MI 49006 ***.*****@*****.*** SUMMARY:
Self-motivated engineer interested in working on multidisciplinary team projects with a focus on aerodynamics and fluids dynamics testing to help improve the efficiency, product design and quality of the product. Proficient on the set-up and conducting experiments in the water and wind tunnels. Experienced with scaled down ground vehicle and vehicle component tests in the wind tunnel.
EDUCATION:
Western Michigan University June 2015
Master of Science in Engineering, Major: Mechanical Engineering, GPA: 3.69 Master’s Thesis Topic:
Oscillating Wind Turbine
Designed a conceptual design of a low speed wind turbine for Wind Tunnel Testing
Constructed the model based on aerodynamic efficiency and structural simplicity
Designed and constructed software to control the model
Video link: https://youtu.be/2SZ-byW-ChU
Western Michigan University April 2011
Bachelor of Science, Major: Aeronautical Engineering, Minor Mathematics GPA: 3.18 Bachelor’s Thesis Topic:
Structural Design of a Soldier Portable Unmanned Aerial Vehicle (UAV)
Designed the structural aspect of a UAV to enable it to carry out the specific missions that was required in the competition
Designed and manufactured the UAV skeleton with the help of CAE tools
Conducted FEA analysis on the prototype to optimize the final design
Represented WMU in AIAA Design Build and Fly in Inter-Collegiate Competition SKILLS:
Ansys(Fluent), AutoCad, SolidWorks, Abaqus FEA, Romax, MathCad, MATLAB, Maple, LabVIEW, Thermal design, Thermoelectric, Wind Tunnel Testing, Water Tunnel Testing, DOE, Minitab, Image Processing and Photogrammetry PUBLICATIONS:
Liu, T., Woodiga, S. A.,Ramasamy, RS Vewen.
“Effects of Yaw and Roll Angles on Skin Friction Topology on Delta Wings” 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, AIAA 2012-0262 Liu, T., M. H. M. Makhmalbaf, Ramasamy, RS Vewen., Kode Sai Kumar, P.Merati
“Skin Friction Fields and Surface Dye Patterns on Delta Wings in Water Flows” Journal of Fluids Engineering, (2015)
Liu, T., Ramasamy, RS Vewen., Kode Sai Kumar
“Global Skin Friction Diagnostics in Junction Flow Using Luminescent Oil” Submitted to AIAA journal for review
Liu, T., Ramasamy, RS Vewen., Radermacher, Ryne., Liou, William.,
“Wind Oscillator for Power Generation”
Submitted to Wind Energy journal for review
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WORK EXPERIENCE:
Western Michigan University, Applied Aerodynamics Lab Research and Development Engineer Jun 2015 – Current
Upgrade the current Oscillating Wind Turbine model for wind tunnel and field testing
Conduct systematic testing to validate the performance of the device
Carry out Photogrammetry and Image processing to validate the systematic testing results
Scaled down ground vehicle testing
Wind Tunnel Testing was performed on scaled down truck models to determine ways to reduce drag
Flow visualization test was conducted using smoke to observe the flow pattern around the model
Conducted tests on the model to collect pressure data for truck companies Micro Laser Assisted Machining Technologies LLC
Development Engineer Sep 2015 – Mar 2016
Conceptualize, design and create 3D model for new products as per customer requirements
Fabricate and optimize the product for final production Graduate Assistant Jan 2013 – Jun 2015
Organized lab resources and performed specific experiments as required
Fabricated testing apparatus and models for experiments
Instructed theory and experimental laboratory sessions for 60 students
Extraction of Skin Friction Fields from Surface Dye Visualizations in Water
Worked on the development of a global skin friction measurement that utilized water based luminescent dye
Carried out dye coating development evaluated different dye media and application techniques
Performed experiments in Water Tunnel to validate the technique and compared it with other techniques
Global Skin Friction Diagnostics in Junction Flow Using Luminescent Oil
Part of an engineering team of three that developed junction flow measurements using a global skin friction diagnostic tool
Performed junction flow measurements to evaluate bodies of varying aspect ratios
Performed Wind Tunnel experiments to compare results with benchmarked models for validation Research Assistant Aug 2011 – Jun 2012
Systematized lab resources, performed and assisted on academic projects and experiments
In charge for fabrication of testing apparatus and models for research
Responsible for laboratory experimental teaching sessions for 30 students
Global Skin Friction Meter
Part of the engineering team that developed a global skin friction measurement method utilizing luminescent oil
Carried out oil coating development to evaluate different oil film viscosities, luminescent dopants and oil film application techniques
Performed experiments in Wind Tunnel to validate the technique and applied it on complex separated flows
Toyota Exhaust Manifold Flow Field Mapping
Part of the team that worked on the design and construction of a test rig to enable Particle Image Velocimetry
(PIV) measurements on the exhaust gas flow of a four cylinder production engine to produce volumetric flow fields
Assisted in performing PIV measurements on the exhaust manifold of a four cylinder production engine
Unmanned Aerial Vehicle (UAV) Airship - (Blimp + Aircraft)
Calculated and re-designed a small scale airship to a larger scale working model
Tested the large scale model for flight performance with the small scale model
Automotive Active Front Grille
Designed and constructed a model from an existed manufactured part for Wind Tunnel Testing
Conducted tests on the model to collect pressure data for an automotive company