1. RESUME
J.PAULRAJ
S/o D. Jeya Singh,
49/A Buckle Puram,
Second Street, paulraaaj@gmail.com
Thoothukudi -628003. Contact No: +919003314844
CAREER OBJECTIVE:
To work in an environment, which is innovative, challenging and rewarding, and which
offers a profound knowledge base to enhance my talent, exposure, and zeal of learning.
EDUCATIONAL QUALIFICATION:
Qualification Year of passing Educational
institution
Board/university Aggregate
Bachelor of
Engineering
(Aeronautical
Engineering)
2015 The Rajas
Engineering
College,
Tirunelveli.
Anna University 71%
12th /Higher
Secondary
2011 Caldwell Higher
Secondary School,
Thoothukudi.
State Board 76.25%
10th /Secondary 2009 Caldwell Higher
Secondary School,
Thoothukudi.
State Board 82.8%
TECHNICAL SKILLS:
 Designing Softwares : CATIA (V5R20), AutoCAD, PROE
 Analysis Softwares : ICEM CFD, Fluent and Gambit
PAPER PRESENNTATION:
 Paper presented in INTERNATIONAL CONFERENCE, titled “AN INNOVATIVE APPROACH TO
DEVELOP PLASMA PANEL COMBUSTOR FOR TURBO JET ENGINES” at Rajas engineering
college, Tirunelveli, Tamilnadu.

2. ACADEMIC PROJECT:
COMMUNICATION SKILLS:
Language Read Write Speak
Tamil   
English   
ACADEMIC ACHIVEMENTS:
 Participated in Workshop, titled “DESIGN AND FABRICATION OF RC DELTA WING
AIRCRAFT” at Bannari Amman Inistitute of technology, Erode, Tamilnadu.
 Participated in Workshop, titled “DESIGN AND FABRICATION OF RC TRI CORPTER” at Bannari
Amman Inistitute of technology, Erode, Tamilnadu.
EXTRA CURRICULAR ACTIVITIES:
 Design and Fabrication of RC Airplanes.
 Photography.
PERSONAL DETAILS:
Father’s Name : D. Jeya Singh.
Date of Birth : 26th Jan 1994.
Gender : Male.
Nationality : India
DECLARATION:
I, hereby, solemnly declare that all the information made above are true and correct to the best of my
Knowledge and belief.
Place: Thoothukudi. Yours Faithfully,
Date: 25-04-2015. (PAULRAJ J)
Project title AN INNOVATIVE APPROACH TO DEVELOP PLASMA PANEL
COMBUSTOR FOR TURBO JET ENGINES.
Project type Final year project
Description Using Engineering skills, modeling of the fighter aircraft plasma panel combustor
for turbo jet engines is done by the using of CATIA software. Analysis is done by
using ICEM CFD.