OBJECTIVE

SHALINI

SURESH

MGR NAGAR, CHENNAI, TAMIL NADU.

989-***-****

adoa0k@r.postjobfree.com

linkedin.com/in/shalini-suresh-

39ab16197/

A self -motivated, hard- working graduate in Aeronautical Engineering looking for a job. I am looking to start my career as an GET which will provides an opportunity to gain knowledge and experience a an Engineer.

EDUCATION

DEGREE/GRADE

INSTITUTION

SCORE

B.E (Aeronautical Engineering) (2017-2021)

JEPPIAAR ENGINERING COLLEGE -CHENNAI.

7.47(6th semester)

Senior- Secondary (Pre-Engineering)

NEW PRINCE MATRI.HR.SEC.SCHOOL-CHENNAI

79%

Secondary (High school)

BELFIELD MATRIC.HR.SEC.SCHOOL-NAGERCOIL

97%

EXPERIENCE

1.WORKSHOP on ROBOTICS by SPIRO SOLUTIONS PRIVATE LTD, Chennai, Tamil Nadu.

2.AVIONICS INTERN at STAR, Surat, Gujarat.

3.Academics tutor for primary class students

SKILLS

ANSYS FLUENT

FUSION 360

PROTEUS

ARDUINO

OPEN ROCKET

PROJECTS

EFFECT OF OPTIMIZED IMPINGEMENT CONFIGURATION WITH EFFUSION COOLING HOLES ON DOUBLE WALL SCHEME: The increase in turbine inlet temperature simultaneously increases the thermal load of the engine components when hot flow gas is being exposed to them. The heat transfer in the double wall technique is being performed by CFD simulations. It helps in analyzing multiple parameters to increase the power output without increasing the pumping power.

STAIC MOTAR TEST PAD DESIGN: A Rocket Motor Static Test Pad is being designed for testing and acquiring the required data for the performance analysis of the high-powered rocket motors

HIGN POWERED ROCKET (HPR)AND NON- PYRO MECHANISM DESIGN: The recovery system for HPR is being designed using non-pyro technique for the HPR and perform simulation in Open Rocket for the HPR design. To develop the avionics recovery system for HPR and log all the important data safely or wirelessly transmit the data during launch.

ACTIVITES/AWARDS

LETTER OF RECOMMADATION from STAR 2021

VOLUNTEEER WORK – TAMIL NADU GLOBAL INVESTEERS MEET 2019

“BEST PROJECT” (EFFECT OF OPTIMIZED IMPINGEMENT CONFIGURATION

WITH EFFUSION HOLES ON DOUBLE WALL SCHEME) in the department of Aeronautical Engineering during the year 2020-21-JEC

Contact this candidate