full final resume
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ARUN KUMAR C 4/38, SALANGUKARA STREET, PARANGIPETTAI, CUDDALORE, TAMILNADU, INDIA-608502 MOBILE: +919994864142 EMAIL: [email protected] CAREER SUMMARY Focused, Analytical professional with strong engineering background complemented by work experience involving research and development projects. Work effectively in both self- managed and team based projects. EDUCATIONAL QUALIFICATION MASTER OF ENGINEERING IN AERONAUTICAL, JUNE 2014 CGPA -7.43/10 (First class) ANNA UNIVERSITY, CHENNAI, TAMILNADU, INDIA. BACHELOR OF ENGINEERING IN AERONAUTICAL, JUNE 2011 CGPA - 7.0/10 (First class) ANNA UNIVERSITY, COIMBATORE, TAMILNADU, INDIA. HIGHER SECONDARY COURSE, APRIL 2007 Percentage - 85/100 (First class) KRISHNASAMY MATRICULATION SCHOOL, CUDDALORE, TAMILNADU, INDIA. SSLC, APRIL 2005 Percentage - 70/100 (First class) SEVAMANDIR MATRICULATION SCHOOL, CUDDALORE, TAMILNADU, INDIA. WORK EXPERIENCE PROJECT ASSISTANT, JUNE 2014 – till date XSOLVE ENGINEERING SOLUTION, COIMBATORE, TAMILNADU, INDIA. Theoretical Design and analysis of Turbo machines Currently working in Axial and Centrifugal Pump project. RESEARCH ASSISTANT, SEP 2011 - SEP 2012 PARK RESEARCH CENTER, COIMBATORE, TAMILNADU, INDIA. Conduct Research, Experimental design, Flow visualization techniques and Performance analysis in Gas Turbine Blade using high speed subsonic wind tunnel. LECTURER, SEP2011 – SEP2012 PARK COLLEGE OF ENGINEERING AND TECHNOLOGY, COIMBATORE, INDIA. Handled subjects, 1. Aircraft repair and maintenance 2.Aircraft structural repair laboratory.
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Transcript of full final resume
ARUN KUMAR C
4/38, SALANGUKARA STREET, PARANGIPETTAI, CUDDALORE, TAMILNADU,
INDIA-608502
MOBILE: +919994864142 EMAIL: [email protected]
CAREER SUMMARY
Focused, Analytical professional with strong engineering background
complemented by work experience involving research and development projects.
Work effectively in both self- managed and team based projects.
EDUCATIONAL QUALIFICATION
MASTER OF ENGINEERING IN AERONAUTICAL, JUNE 2014 CGPA -7.43/10 (First class) ANNA UNIVERSITY, CHENNAI, TAMILNADU, INDIA.
BACHELOR OF ENGINEERING IN AERONAUTICAL, JUNE 2011 CGPA - 7.0/10 (First class) ANNA UNIVERSITY, COIMBATORE, TAMILNADU, INDIA.
HIGHER SECONDARY COURSE, APRIL 2007 Percentage - 85/100 (First class) KRISHNASAMY MATRICULATION SCHOOL, CUDDALORE, TAMILNADU, INDIA.
SSLC, APRIL 2005 Percentage - 70/100 (First class) SEVAMANDIR MATRICULATION SCHOOL, CUDDALORE, TAMILNADU, INDIA.
WORK EXPERIENCE
PROJECT ASSISTANT, JUNE 2014 – till date XSOLVE ENGINEERING SOLUTION, COIMBATORE, TAMILNADU, INDIA.
Theoretical Design and analysis of Turbo machines
Currently working in Axial and Centrifugal Pump project.
RESEARCH ASSISTANT, SEP 2011 - SEP 2012
PARK RESEARCH CENTER, COIMBATORE, TAMILNADU, INDIA.
Conduct Research, Experimental design, Flow visualization techniques and
Performance analysis in Gas Turbine Blade using high speed subsonic wind tunnel.
LECTURER, SEP2011 – SEP2012
PARK COLLEGE OF ENGINEERING AND TECHNOLOGY, COIMBATORE, INDIA. Handled subjects, 1. Aircraft repair and maintenance 2.Aircraft structural repair
laboratory.
SOFTWARE SKILLS
ANSYS WORKBENCH (STRUCTURAL),
ANSYS CFX, FLUENT
ANSYS DESIGN MODELER
HYPERMESH (intermediate level)
CATIA V5(PARTDESIGN, ASSEMBLY,DRAFTING)
PROJECT DETAILS
RESEARCH PROJECT: LOW REYNOLDS NUMBER PERFORMANCE OF
SMALL ENGINE TURBINE
DESCRIPTION: Low Reynolds number performance of a typical small helicopter engine
blade was tested in a low speed cascade wind tunnel. The pressure distribution and the wake
profiles were measured at various incidences and for varying Reynolds numbers. When the
Reynolds number was decreased the laminar separation bubble on the suction side of the
blade increased both in stream wise and wall normal directions accounting for higher losses.
It was observed that irrespective of the incidence angle there exist a critical Reynolds
number, below which there was a sudden rise in the profile loss. This project was funded by
Aeronautical Research and Development Board (AR&DB, India) and was done at PARK
Research Centre.
M.E PROJECT: OPTIMIZATION OF INTERNALCOOLING CONFIGURATION IN
A NOZZLE GUIDE VANE
DESCRIPTION: The main aim of this project is to reduce the temperature of the turbine
blade by increasing heat transfer between the blade and the cold air. Turbine blade inter part
is split into four channel and the ribs turbulator is placed in the leading edge channel because
temperature is higher in that region. Rib Turbulator are used to reduce pressure and separate
the flow inside the blade and it also increase the optimum heat transfer.
Software used: ICEM-CFD, ANSYS- CFX)
Project guide: Mr.S.V. REDDY (HAL, BANGALORE)
B.E PROJECT : DESIGN AND ANALYSIS OF SOLID ROCKET MOTOR CASING
DESIGN FOR A SATELLITE LAUNCH VEHICLE
DESCRIPTION : The main theme of our project is to design a solid rocket motor case, its
dome structure and its attachment. To design of solid rocket motor case, some assumption are
considered based on advantage and disadvantage. In this project, we selected the cylindrical
case as a design structure. Torispherical dome and Segment joint straight pin attachment used
in the conceptual design of the solid rocket motor case. We selected MARAGING STEEL
grade250 material for the entire design case.
Software used: CATIA V5, ANSYS.
Project guide : Mr. S.MURUGESAN (Retd Scientist from VSSC/ISRO).
EXTRACURRICULAR ACTIVITIES
Secured first place in SDAT district Hockey tournament.
Secured first place in Coimbatore zone Hockey championship.
Secured first place in Zonal Hockey tournament conducted by Anna university
REFERENCE
Dr.A.P.HARAN (Group Director, Afterburner Division, GTRE, Bangalore (Retd.)),
Head of Aeronautical Engineering,
Park College of Engineering, Coimbatore.
Phone no: 09789452202
Email:[email protected]
MR. MUTHUKUMAR
Assistant professor,
Park College of Engineering and Technology
Phone no: 08903534785
Email:[email protected]
