Help
Home
Search the Forum
You are Here :
Forum
Careers
Media TV Cinema NewsPaper
The Writers Block TWB Bangalore : Technical Writer
Ask Question / Post resume
Post a reply to the thread:
The Writers Block TWB Bangalore : Technical Writer
Your Message
Your Username:
Click here to log in
Notes:-
1) You can copy and paste your full resume in the box below.
2) Or you can ask your question. We try to answer, as far as possible.
Title:
[QUOTE=Guest-IJT;127869][b]Name [/b]: Thileepanragu R [b]Email [/b]: thileepan_ragu AT yahoo.co.in [b]Designation / Skillset[/b] : Technical writer As an aeronautical engineer, I am perfect in engineering principles, and aircraft systems and structural components. In addition, I have excellent knowledge in S1000 & ATA standards. Also I have very good knowledge about AutoCAD, Gambit and Fluent. My key strength includes leadership, creativity, troubleshooting skills and quick problem solving ability. I believe that I could make significant contribution to your firm. If you are interested in interview, please contact me at 9739517321 or e-mail me on thileepan.ragu AT gmail.com. Thank you for reading my cover letter and resume. Sincerely, THILEEPANRAGU R. [u][b]Resume[/b][/u] : Objective To obtain a position where I can contribute my skills as an experienced professional, resulting in a mutually beneficial growth relationship between my employer, my team and myself. Experience [b]Client [/b]: BOMBARDIER AEROSPACE, CSeries. [b]PROJECT PROFILE [/b]: [b]Manuals [/b]: AMP, SDS, ASRP & IPDP. [b]Standards [/b]: s1000d & ATA. [b]Tools [/b]: SAP Workbench, Arbortext editor and CATIA ENOVIA. [b]Role [/b]: Author – Mechanical. - 1 Year 4 months of Experience as Technical writer [b]PROFESSIONAL SUMMARY [/b]: - Knowledge in different kinds of manuals like AMP, SDS, ASRP, IPDP & ANDTP - Exposure to Simplified Technical English standard ASD-STE 100 - Knowledge on S1000D Standards and Business rules - Knowledge on Aerospace Standards ATA100 & ispec 2200. - Analyzing and Validation of “Change Drivers” like MODSUM (Modification Summary), MCR (Manual Change Request) and SB (Service Bulletin) for the respective Data Modules by doing Impact Analysis and incorporating the corresponding changes on the data modules based on the Change Drivers provided by the Manufacturer, Service provider and Airliner. [b]NATURE OF JOB [/b]: - Creating and Revising IPDP (Illustrated Parts Data Publication) data modules by incorporating change drivers like MODSUM, MCR, SB and RIL (Reference Instruction Letter) etc. - Use of SAP (Material Management) for creating and changing material data found after the analysis of engineering documents. Use of SAP database for creating, editing the parts list. - Use of S1000D and AECMA (European Association of Aerospace Industries) Simplified Technical English standards for editing the procedure in data modules. Associate Consultant Capgemini Business Services (India) Limited 15-Feb-2010 to till date - CFD Analysis of heavy vehicles to increase the fuel economy by reduction the drag [b]RESPONSIBILITIES [/b]: - CFD Analysis of Low Re-airfoils for Micro Air Vehicles (MAV). Education Projects Prediction of Hysteresis Associated With a NACA 0012 Airfoil Computations for 2D unsteady flow past a NACA 0012 airfoil are carried out for increasing and decreasing angles of attack, using FLUENT code. Hysteresis in the aerodynamic coefficients is observed for a small range of angles of attack close to the stall angle. This is due to the variation in the location of the separation point on the upper surface of the airfoil during the increasing and decreasing angles of attack. For increasing angle, the separation point moves gradually towards the leading edge and for decreasing angle, the movement is contrary. Control of the Onset of the Stall Angle on an Aircraft Wing with Vortex Generators The influence of the addition of vortex generators on an aircraft wing with NACA 0012 cross section is analyzed using FLUENT simulations. In addition to increasing the lift coefficient, the addition of vortex generators increases the stalling angle also. The three-dimensional wing with vortex generators is modeled in AUTOCAD. Shock Wave Boundary Layer Interaction in Supersonic Inlets The fluid flow behavior at the interaction between the oblique shock wave and the boundary layer formed on the surface of the inlet is studied by performing numerical simulations using FLUENT. Publication Thileepanragu R, Anand U, Sudhakar Y, Gopinathan V.T., Rajasekar R. “Passive Flow Control over NACA0012 Aerofoil Using Vortex Generators”, Proceedings of the 37th National and 4th International Conference on Fluid Mechanics and Fluid Power, FMFP 2010, IIT Madras, Paper Accepted. Research Associate Park Research Center 01-Jun-2009 to 11-Feb-2010 Course Year Of Completion Institution Board/ University Marks % B.E., (Aeronautical Engg.) 2009 Park College of Engineering and Technology, Coimbatore. Anna University 72.12 12th 2005 Government Boys Higher Secondary School, Pattukkottai. State Board 88 10th 2003 Government Higher Secondary School, Pallathur. State Board 91 Computer Skills [b]- Design [/b]: AutoCAD, Gambit [b]- Analysis [/b]: FLUENT [b]- Publishing [/b]: MS-OFFICE [b]- Operating systems [/b]: Windows Extra Curricular Activities - Second Place in CIT Kabaddi trophy - Third Place in Anna University Zonal Kabaddi tournament - Lead the team and Won Fourth Place in Tamil nadu Inter-Engineering Sports (TIES) Kabaddi tournament - Sports secretary for the Department of Aeronautical Engineering. (THILEEPANRAGU.R) ------------------------------------------------------- [b]More Information about this submission and submitter [/b]:- ___________________________________________________ [b]Submission ID [/b]: 4268992 [b]Date & Time [/b]: 18th Jun 2011 6:44 AM (UTC) [b]IP Address [/b]: 123.238.83.46 [b]Browser Info [/b]: Mozilla/5.0 (Windows NT 5.1; rv:2.0.1) Gecko/20100101 Firefox/4.0.1 Predicted Country : India[/QUOTE]
