Immanuvel D ME CV
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Immanuvel D is seeking entry-level managerial positions in R&D or production. He has a M.E. in Aeronautical Engineering and experience working on projects for DRDO and NAL. Currently he is a senior research fellow at PSG College of Technology. He has skills in CAD, CFD, and structural analysis software and experience in design, simulation, and computational analysis. He is interested in heat transfer, turbomachinery, and aerodynamics.
Immanuvel D ME CV
- 1. Name : Immanuvel D Mobile No : +91-9894711831 Email id : imansundar@gmail.com OBJECTIVES: Senior Research Fellow at PSG, Coimbatore, in quest of entry level managerial assignments in R&D/ Production with an organization of repute PROFILE SUMMARY: Effectively handled Projects of "Defence Research and Development Laboratory, Hyderabad", "National Aerospace Laboratories, Bangalore", "Versa Drives Pvt.Ltd, Coimbatore". M.E. in Aeronautical with good Experience in handling Design & Simulation Software's. Passionate learner with an ability to work under pressure and meet the deadlines. Able to Work Independently or cooperatively as part of a team. WORK EXPERIENCE: Senior Research Fellow/ CAE Analyst (Jan 2015 - Current) PSG College of Technology, Coimbatore S.No Project Title Type Agency Duration Status 1. DEVELOPMENT OF REGENERATIVE STORAGE AIR HEATER DESIGN MODEL R&D Defence Research and Development Laboratory, Hyderabad. Dec 2014 - Jan 2016 Completed 2. COMPUTATIONAL AND STRUCTURAL ANALYSIS OF CEILING FAN R&D Versa Drives Pvt.Ltd, Coimbatore. April 2016 - May 2016 Completed Assisted in Organising Conferences, workshops conducted by Department of Mechanical Engineering. Handled purchases, Bill settlements and other office related works. TECHNICAL QUALIFICATION: Hands on knowledge in, Modelling Tools : SolidWorks, Ansys-Design Modeler, Catia, Unigraphics, MSc-Patran. Meshing Tools ; Ansys-Icem, Hypermesh. Computational Analysis Tools : Ansys-Fluent, Ansys-CFX. Structural Analysis Tools : Ansys-Structural, MSc-Nastran. AREAS OF INTEREST: Heat Transfer Turbomachinery Aerodynamics ACADEMIC DETAILS: M.E. in Aeronautical from Nehru Institute of Engineering and Technology, Coimbatore, Anna University with 6.6 / 10 CGPA in 2014 B.E. in Aeronautical from Gojan School of Business and Technology, Chennai, Anna University with 66% in 2011 12 th from St. Pauls Matriculation Higher Secondary School, Kovilpatti, State Board with 74% in 2007 10 th from St. Pauls Matriculation Higher Secondary School, Kovilpatti, Matric with 83% in 2005
- 2. JOURNALS PRESENTED: 1. Stress analysis and weight optimization of a wing box structure subjected to flight loads on IJES, Volume 3, Issue 1, Pages 33-40, 2014. PAPERS PRESENTED: 1. Control Of Asymmetric quad rotor on international conference held on Thiruvalluvar college of engineering and Technology, Vandavasi. 2. Analysis of bird strike and its avoidance Techniques on national level technical conference (NIACE-13),NIET, Coimbatore. ACADEMIC PROJECTS: Masters in Engineering National Aerospace Laboratories, Bangalore (Jun 2013 - Nov 2014) Title: A Comparative Study Of Two And Three Bladed Mini UAV Propellers Having Same Solidity Dissertation of the project: National Aerospace Laboratories (NAL) is one of the premiere institute for aerospace R&D under Council of Scientific and Industrial Research (CSIR). CSIR-NAL has been involved in the development of a 300 mm & 450 mm span Fixed wing Micro Air Vehicle (MAV) and a 2 Kg class mini unmanned aerial vehicle (UAV) for the past few years. Propulsion system for most of the mini UAVs uses fixed pitch propeller as a means for producing thrust. These propellers operates at very low Reynolds numbers which is mostly below 100,000. Designing of efficient propellers and wings at this low Reynolds numbers is extremely difficult, as in this regimes the propeller has to face the dominance of viscous forces and laminar boundary layer separations. In mini UAV design, consideration of efficiency is most important, as high efficiency of the propeller leads to higher endurance which is the most important thing in designing of a mini UAVs. It is a common assumption that number of blades in the propeller has a small effect of efficiency. But as the number of blades increases it leads to more even distribution of thrust and power even in the wake flows. The choice of no blades for the selection or design of the propeller is a tricky situation for a mini UAV designer. Many parameters such as power consumption, blade solidity, advance ratio etc. will get influenced while trying to increase or decrease the number of blades of a propeller. In the present work two propellers namely, two bladed 11 inch diameter and three bladed 9.5 inch diameter propeller are designed using minimum induced loss method for a mini UAV. The blade solidity and design advance ratio of both propeller is maintained same by adjusting the diameter, chord length and propeller rotational speed. Performance evaluation of both the propellers for different operating conditions are carried out using Simple blade element momentum theory and 3D CFD analysis using ANSYS FLUENT. The performance of both the propeller are compared and discussed in the present study. Bachelors in Engineering Title: Creating A Large Turbulence Inside The Combustion Chamber Using Perforated Plate Dissertation of the project: The objective of the project was to develop a can annular combustion chamber for high efficiency & performance. This can be done by creating a large turbulent flow inside a combustion chamber by placing a thin perforated plate in combustor area. By placing a thin perforated plate in the mixing region, the air-fuel got rapidly mixed as the perforated holes increases turbulence thereby the Static pressure & combustion efficiency. The modelling of the combustion system was done in CATIA V5, unstructural meshing done in Ansys-Gambit and computational analysis were carried out using Ansys-Fluent.
- 3. WORKSHOPS ATTENDED: YEAR NAME OF WORKSHOP UNIVERSITY/ COLLEGE TOPICS COVERED 2010 RC models Madras Institute of Technology, Chennai. Training in Construction, assembling, Flying session, Maintenance of models 2010 Advanced composite materials Sri Ram College of Engineering, Chennai. Composite Hybrids, Composite damage tolerance & maintenance INDUSTRIAL VISITS: COMPANY REPUTATION ADDRESS AGNI Aviation Supplier of Aircraft components and Aircraft Equipments, Aircraft engines. Hangar No.2, Jakur aerodrome, Bengaluru-560064 India. Govt Flying club Training to Fixed wing, Rotary wing (Helicopters), CPL as well as PPL licences. Govt flight training school, Jakur Aerodrome, Bengaluru-560064 India. PERSONAL DETAILS: Father name : David G Date of Birth : 17-06-1990 Sex : Male Nationality : Indian Permanent Address : 11E, Blessing cottage, Behind Shanmuga theatre, Ettayapuram Road, Kovilpatti-628501. Marital Status : Single Languages Known : Tamil, English, Hindi (Basic). Hobbies : Photography, listening to music Extra software skills : MS-office package, Adobe Photoshop. REFERENCES: 1. Lt. Dr. S. Babu, Assistant Professor (S.G), School of Energy, Dept. of Mechanical Engineering, PSG College of Technology, Coimbatore - 641 004. Mob: +91-9487248598 2. Prof. V. Sankar, Head of the Department, Department of Aeronautical, Nehru Institute of Engineering and Technology, Thirumalayampalayam, Coimbatore-641 105. Mob: +91-9842336409 I do hereby confirm that the information given above is true to the best of my knowledge. Place : Coimbatore Yours Truly, Date : 23/05/2016 (Immanuvel D)