Engineering Turbine
Resume:
CAREER OBJECTIVE:
To build a long-term career in a progressive institution bringing forth my precise teaching and research oriented skills to solve problems in a creative and effective manner in a challenging position.
EDUCATIONAL QUALIFICATION:
• M. Tech in Thermal Engineering at Karunya Institute of Technology and Sciences in Coimbatore with a CGPA of 7.97 (10.0 grading scale) till Third semester.
• Bachelors of Technology Degree in Aerospace Engineering (B. Tech) from Karunya Institute of Technology and Sciences in Coimbatore with an overall CGPA of 7.36 (10.0 grading scale) in the year 2017.
• Graduated High School, twelfth grade at Bethlehem higher secondary school with 87.8% in the year 2013.
• Completed tenth grade at St. Johns school with 86% in the year 2011. SKILLS:
Communicational and Organizational skills:
• Good communicational skills.
• Ability to lead and be a part of a team and interact in a diverse team.
• Can adapt to any environment very easily.
• Can effectively communicate (both verbal and written) and put across ideas to coworkers.
• Ability to think precisely and curious to learn. Technical proficiency:
• Good understanding on fundamental concepts of Aerospace & Mechanical Engg.
• Areas of interest in the field of Thermal and Design of Heat pipes C.V GINU SARA
25 /47A Manatharai vilai,
Palliyadi – 629169
Kanayakumari dist.,
addohm@r.postjobfree.com
Software proficiency:
• Familiar with Solid works and Gambit fluent
• Completed a course on ANSYS WB and ANSYS CFX
International Journal Publications: (under preparation) 1. Ginu Sara, L. Godson Asirvatham, “Effect of filling ratio and tilt angle on the performance of cross flow heat pipe”, International Journal of Heat and Mass Transfer,
(under preparation).
2. Ginu Sara, L. Godson Asirvatham, “Effect of tilt angle on cross flow heat pipe using Graphene nanofluid for electronic cooling applications”, Experimental Thermal and Fluid Science, (under preparation).
3. Ginu Sara, L. Godson Asirvatham, “Effect of coating and tilt angle on the performance of cross flow heat pipe”, International Communications in Heat and mass transfer”,
(under preparation).
ADDITIONAL TRAINING:
Workshops and Symposiums attended:
• RC Aircraft Design Fabrication and Flying Organized by Aerotrix, Bangalore
• National Level One Day Seminar on Composite Material in Aerospace Applications.
• National Level One Day Seminar on Unmanned Aerial System-Recent Trends and Future Prospects.
• National level workshop sponsored by CSIR On Futuristic material and energy storage system
Internships and Trainings Undertaken:
• Airport Authority of India, Chennai.
• Aero Pioneers Technologies Bangalore.
Academic Projects:
PROJECT 1:
Title: Theoretical analysis of Floats and Parachutes for an Aircraft. Description: During recent years, lot of flight crashes have taken place. In order to consider the safety of passengers, Theoretical calculation on floats and parachutes are done. For emergency, once the passenger seat is ejected, parachute attached with the seat opens at the particular height and time which helps in safe landing. In order to avoid the jerks while reaching the ground, floats are attached to the seat so that the passenger can reach the ground safely.
PROJECT 2:
Title: Performance of cross flow heat pipe using Graphene nanofluid for electronic cooling applications.
Description: The new electronic devices put forward the challenge of efficient cooling when the heat loads are rapidly increasing. The life span of electrical devices decreases as their operating temperature increases. In order to provide the solution for this problem, a Cross flow heat pipe which can work at any inclination and orientation for effective cooling in electronic devices had been design and fabricated. Novelty of the design is it have one evaporator and four condensers with ten fins at each loop, which make the heat transfer more efficient. Different nanofluids are used to improve the heat transfer. Compared to other nanofluids, Graphene nanofluid has high thermal conductivity. So based on the properties graphene nanofluid was selected with the optimum filling ratio of 60% for different concentration
(0.01%,0.03%,0.05%) as studied. The experiment was conducted with the heat load ranging from 20W to 160W. Cross flow heat pipe with heat load of 20Wto 160W are used in different fields for various applications especially in the field of aerospace. The efficiency obtained is 93.5% for 0.05%.
PROJECT 3:
Title: Heat pipe turbine for power generation Applications. Description: A new concept for power generation from solar, geothermal or other available low grade heat sources using heat pipe turbine. The basis of the heat pipe turbine is the modified thermosyphon cycle with the excellent heat and mass transfer characteristics which incorporates a turbine in adiabatic region. The heat pipe turbine which has closed vertical cylinder with the evaporator an insulated adiabatic region and a condenser. Conservation of enthalpy difference to kinetic energy is achieved through the nozzle. The mechanical energy developed by the turbine can be converted in to electrical energy by direct coupling the electric generator.
EXPERIENCE:
I have been working currently in Dhanalakshmi Srinivasan engineering college for past 9 months. The following subjects are handled:
Propulsion
Space science
Introduction to aerospace
Flight system and instrumentation
Aerodynamics
EXTRACURRICULAR ACTIVITIES:
• Member of National Service Scheme and Rotaract Club.
• Participated in workshop on Leadership in association with Global Leadership Summit.
• Participated in the One Day Workshop on Environmental and Wealth Organized by the Nature club.
PERSONAL DETAILS:
Name : C.V Ginu Sara
Date of Birth : Sept 19,1995
Languages known : English, Tamil (read, speak and write) Hobbies : Reading, enjoying nature.
DECLARATION:
I hereby declare that all the above mentioned statements are correct and true to the best of my knowledge.
DATE:
PLACE : C.V GINU SARA
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